+ All Categories
Home > Documents > Experimental Forward Flight Rotor Performance Testing From ...

Experimental Forward Flight Rotor Performance Testing From ...

Date post: 04-Feb-2022
Category:
Upload: others
View: 4 times
Download: 0 times
Share this document with a friend
114
NASA/CR2019220229 Experimental Forward Flight Rotor Performance Testing From Terrestrial to Martian Atmospheric Densities Brenda Natalia Perez Perez, Geoffrey A. Ament, and Witold J. F. Koning Science and Technology Corporation Ames Research Center, Moffett Field, California Click here: Press F1 key (Windows) or Help key (Mac) for help June 2019
Transcript

NASA/CR—2019–220229

Experimental Forward Flight Rotor Performance Testing From Terrestrial to Martian Atmospheric Densities

Brenda Natalia Perez Perez, Geoffrey A. Ament, and Witold J. F. Koning

Science and Technology Corporation

Ames Research Center, Moffett Field, California

Click here: Press F1 key (Windows) or Help key (Mac) for help

June 2019

NASA STI Program ... in Profile

Since its founding, NASA has been dedicated

to the advancement of aeronautics and space

science. The NASA scientific and technical

information (STI) program plays a key part in

helping NASA maintain this important role.

The NASA STI program operates under the

auspices of the Agency Chief Information

Officer. It collects, organizes, provides for

archiving, and disseminates NASA’s STI. The

NASA STI program provides access to the NTRS

Registered and its public interface, the NASA

Technical Reports Server, thus providing one of

the largest collections of aeronautical and space

science STI in the world. Results are published in

both non-NASA channels and by NASA in the

NASA STI Report Series, which includes the

following report types:

TECHNICAL PUBLICATION. Reports of

completed research or a major significant

phase of research that present the results of

NASA Programs and include extensive data

or theoretical analysis. Includes compilations

of significant scientific and technical data

and information deemed to be of continuing

reference value. NASA counterpart of peer-

reviewed formal professional papers but has

less stringent limitations on manuscript length

and extent of graphic presentations.

TECHNICAL MEMORANDUM.

Scientific and technical findings that are

preliminary or of specialized interest,

e.g., quick release reports, working

papers, and bibliographies that contain

minimal annotation. Does not contain

extensive analysis.

CONTRACTOR REPORT. Scientific and

technical findings by NASA-sponsored

contractors and grantees.

CONFERENCE PUBLICATION.

Collected papers from scientific and

technical conferences, symposia, seminars,

or other meetings sponsored or co-

sponsored by NASA.

SPECIAL PUBLICATION. Scientific,

technical, or historical information from

NASA programs, projects, and missions,

often concerned with subjects having

substantial public interest.

TECHNICAL TRANSLATION.

English-language translations of foreign

scientific and technical material pertinent to

NASA’s mission.

Specialized services also include organizing

and publishing research results, distributing

specialized research announcements and feeds,

providing information desk and personal search

support, and enabling data exchange services.

For more information about the NASA STI

program, see the following:

Access the NASA STI program home page

at http://www.sti.nasa.gov

E-mail your question to [email protected]

Phone the NASA STI Information Desk at

757-864-9658

Write to:

NASA STI Information Desk

Mail Stop 148

NASA Langley Research Center

Hampton, VA 23681-2199

This page is required and contains approved text that cannot be changed.

NASA/CR—2019–220229

Experimental Forward Flight Rotor Performance Testing From Terrestrial to Martian Atmospheric Densities

Brenda Natalia Perez Perez, Geoffrey A. Ament, and Witold J. F. Koning

Science and Technology Corporation

Ames Research Center, Moffett Field, California

National Aeronautics and

Space Administration

Ames Research Center

Moffett Field, CA 94035-1000

June 2019

ACKNOWLEDGMENTS

The authors would like to thank Farid Haddad for his expertise in electronics and controls during

experimental setup, Ken Smith for operation of the PAL vacuum facility, Eduardo Solis for

scanning the 40x22 AWT rotor for RotCFD simulation, Larry Meyn for his expertise with the

data reduction, Larry Young for originally inspiring the idea of forward flight testing under

Martian conditions, Haley Cummings for her invaluable feedback and support throughout the

project, and William Warmbrodt for his continued support and guidance on the project. Lastly, a

thank you to the 2017–2018 Aeromechanics Interns for their support during data collection.

Available from:

NASA STI Support Services National Technical Information Service

Mail Stop 148 5301 Shawnee Road

NASA Langley Research Center Alexandria, VA 22312

Hampton, VA 23681-2199 [email protected]

757-864-9658 703-605-6000

This report is also available in electronic form at

http://ntrs.nasa.gov

iii

TABLE OF CONTENTS

LIST OF FIGURES .........................................................................................................................v

LIST OF TABLES ...........................................................................................................................v

NOMENCLATURE ...................................................................................................................... vi

SUMMARY .....................................................................................................................................1

INTRODUCTION ...........................................................................................................................1

TEST FACILITY .............................................................................................................................2

Planetary Aeolian Laboratory ..................................................................................................... 2

Martian Surface Wind Tunnel ..................................................................................................... 2

TEST INSTALLATION, HARDWARE, AND DATA COLLECTION ........................................4

Hardware Installation .................................................................................................................. 4

Test Hardware ............................................................................................................................. 5

Data Collection ............................................................................................................................ 8

POST-PROCESSING ......................................................................................................................8

Data Acquisition .......................................................................................................................... 8

Initial Post-Processing ................................................................................................................. 9

Zero Corrections .......................................................................................................................... 9

Weight Tares ............................................................................................................................. 10

Aerodynamic Tares ................................................................................................................... 11

Torque Tares ............................................................................................................................. 11

Absolute Pressure Offset Correction ......................................................................................... 11

Force and Moment Calculations ............................................................................................... 14

Rotor Configurations ................................................................................................................. 14

Drag and Side Force Contributions to Measured Moments ...................................................... 15

PRESENTED DATA .....................................................................................................................16

Pressure Decrease ...................................................................................................................... 16

Constant Pressure ...................................................................................................................... 17

Pressure Drift............................................................................................................................. 17

Pressure Increase ....................................................................................................................... 18

iv

TABLE OF CONTENTS (cont.)

CONCLUSIONS............................................................................................................................18

FUTURE WORK ...........................................................................................................................18

Wind Tunnel Construction ........................................................................................................ 18

REFERENCES ..............................................................................................................................19

APPENDIX A—ISOLATED ROTOR HARDWARE TECHNICAL DRAWINGS ...................21

APPENDIX B—CORRECTED DATA ........................................................................................35

v

LIST OF FIGURES

Figure 1. Planetary Aeolian Laboratory (PAL). ........................................................................... 3

Figure 2. PAL Martian Surface Wind Tunnel. ............................................................................. 3

Figure 3. Left and right images show two- and four-bladed rotor configurations tested

in the MARSWIT test section, respectively. ................................................................ 4

Figure 4. Left image shows two-bladed rotor at a 0-degree shaft angle; right image shows

two-bladed rotor at a –14-degree shaft angle. ............................................................... 4

Figure 5. Two-bladed rotor at a –14-degree shaft angle, looking downstream of the

test section. .................................................................................................................... 5

Figure 6. Side profile of the 43-foot-long MARSWIT. ............................................................... 5

Figure 7. Hardware and sensor installation within the MARSWIT test section. ......................... 6

Figure 8. Weight tare values for load cells 1, 2, and 3.. ............................................................. 10

Figure 9. Torque tares at reduced pressures. .............................................................................. 12

Figure 10. Torque tares at 1 atmosphere. ..................................................................................... 12

Figure 11. Setra 204 offset vs. pressure. ...................................................................................... 13

Figure 12. Load cell locations. Bolt holes are on a radius of 5.455 inches. ................................. 14

Figure 13. Rotor thrusting up in forward flight, view from ceiling. ............................................ 15

Figure 14. Drag contribution to pitching moment, body-axis system.. ........................................ 15

LIST OF TABLES

Table 1. Weight tare fit coefficients with standard deviations ................................................. 10

Table 2 Readings of automated pressure calibrator vs. Setra 204. .......................................... 13

Table 3. Executed test matrix .................................................................................................... 16

Table 4. Test RPMs for each configuration, as PAL pressure was evacuated. The exact

pressure the chamber was evacuated to varied throughout testing. ............................ 17

Table 5. Range of tested RPM for two- and four-bladed rotors as pressure was held in

the vacuum chamber. .................................................................................................. 17

Table 6. Range of tested RPM for each configuration. ............................................................. 17

Table 7. RPM for the four-bladed configuration, as PAL pressure was evacuated. ................. 18

vi

NOMENCLATURE

CFD Computational Fluid Dynamics

DAS Data Acquisition System

IR infrared

JPL Jet Propulsion Laboratory

MARSWIT Martian Surface Wind Tunnel

MH Mars Helicopter

PAL Planetary Aeolian Laboratory

RAP Resonance Assessment Profile

UAV Unmanned Aerial Vehicle

point Point number within a run during testing

run Run number during testing

SVS NASA Ames Thermal Physics Facility’s Steam Vacuum System

CMx (~) Roll moment coefficient

CMy (~) Pitch moment coefficient

CP (~) Power coefficient

CT (~) Thrust coefficient

D (lbf) Rotor drag force

FM (~) Figure of merit

Mtip (~) Advancing tip Mach number

Mx (in-lb) Roll moment

My (in-lb) Pitch moment

n (~) Number of propellers fixed to the rotor shaft during testing

P (hp) Power

P (millibar) Chamber pressure in the PAL

Pi (hp) Ideal power

Q (ft-lb) Torque applied by the motor

Re.75 (~) Reynolds number at a radial station of 0.75

RPM (~) Revolutions per minute

S (lb) Rotor side force

T (⁰F) Temperature in the PAL

T (lb) Thrust measured by load cells

V (ft/s) Free stream velocity

(ft2/s) Kinematic viscosity of air

(deg) Azimuth angle of thrust vector location, measured counterclockwise from 0-degree

azimuth

(lb/ft3) Air density in the PAL

1

EXPERIMENTAL FORWARD FLIGHT ROTOR PERFORMANCE TESTING FROM TERRESTRIAL TO MARTIAN

ATMOSPHERIC DENSITIES

Brenda Natalia Perez Perez, Geoffrey A. Ament, and Witold J. F. Koning1

Ames Research Center

SUMMARY

With the recent interest in Martian exploration using Unmanned Aerial Vehicles (UAVs), an

experimental study was conducted to investigate rotor performance at Martian atmospheric

conditions. Both simulation and testing of rotors are vital for the evaluation of rotor performance

and behavior, especially for operations at Martian atmospheric densities and pressures. Testing

and measuring rotor forward flight performance at Martian atmospheric conditions is a relatively

unexplored area. Therefore, an experimental study was performed in a wind tunnel to investigate

helicopter forward flight performance and to demonstrate successful rotor operation at Martian

atmospheric densities. This work was a continuation of the first-ever wind tunnel test of a

simulated rotorcraft in forward flight at Martian atmospheric densities. A test was conducted in a

facility that could be evacuated to the atmospheric pressure and density of Mars. A 40-inch-

diameter rotor, roughly approximating the scale of the proposed Mars Helicopter (MH) design by

the NASA Jet Propulsion Laboratory (JPL), was tested in forward flight at Mars’ atmospheric

pressure at the NASA Ames Planetary Aeolian Laboratory (PAL). In this forward flight testing,

the drive system of the Martian Surface Wind Tunnel (MARSWIT) was never turned on. The

goal of this experiment was to collect rotor thrust, rotational speed, power, torque, and wind

speed measurements. Subsequently, these results can be used for correlation with simulated cases

using a mid-fidelity Computational Fluid Dynamics (CFD) simulation. Rotor thrust and power

seem to decrease approximately proportional to the decrease in density. However, the Reynolds

number has an effect on rotor performance that might also be contributing to the change in thrust

and power. This effect plays a vital role in rotor performance at reduced pressure that cannot be

neglected in the simulation. Despite the challenges involved in testing at a large difference of

atmospheric densities between Earth and Mars, repeatable data is obtained in all the

measurements at Martian atmospheric conditions.

INTRODUCTION

The work presented here is an extension of the initial study performed by Ament, Koning, and

Perez Perez [1]. Information is repeated in this report for the benefit of the reader. However,

sections have been modified to describe the distinctive aspects of this work.

1 Science and Technology Corporation, NASA Research Park, Moffett Field, CA 94035.

2

In the interest of exploring and learning more about our solar system, NASA has performed

several unmanned missions to Mars. Among these successes, various missions to Mars have

allowed for close examination of the Martian surface, and one rover is still in operation today.

Unfortunately, because of Mars’ rocky terrain and communication delays between Earth and

Mars, it can be difficult to efficiently move around on the Martian surface. In an effort to help

resolve these issues, the NASA Jet Propulsion Laboratory (JPL) is developing a Mars Helicopter

(MH) in collaboration with AeroVironment Inc., NASA Ames Research Center, and NASA

Langley Research Center, to create a low-altitude Unmanned Aerial Vehicle (UAV) to scout in

the vicinity of the rover and explore the red planet [2].

Considering the drastic differences in gravity and atmospheric conditions between Earth and

Mars, many obstacles must be overcome when designing a flight vehicle for Martian exploration.

Because the gravity on Mars is roughly one-third that of Earth’s, a flight vehicle weighs less on

Mars than on Earth; consequently, a flight vehicle would need less thrust to become airborne.

However, the reduced thrust required from a lighter vehicle is undermined by the drastic

reduction in atmospheric density, which is approximately 1 percent of Earth’s atmospheric

density. In addition, the reduction in temperature, specific heat ratio, and atmospheric gas

constant reduce the speed of sound considerably. Further, the low Reynolds number for a rotor

operating in a Martian atmosphere has a high impact on rotor performance because of possible

early flow separation on the blade [3].

TEST FACILITY

Planetary Aeolian Laboratory

The Planetary Aeolian Laboratory (PAL) is a 98.5-foot-high, 141,259-cubic-foot-volume, near-

vacuum facility capable of conducting experiments under atmospheric conditions ranging from

Earth’s atmosphere, approximately 1 bar, down to 5.5 millibars [4], which is less than the

atmospheric pressure of Mars. The facility can be evacuated to its minimum pressure of

5.5 millibars in about 45 minutes, an operation performed by the NASA Ames Thermal Physics

Facility’s Steam Vacuum System (SVS) [4].

At all atmospheric conditions, the PAL chamber atmosphere composition is that of Earth’s; for

noncritical Mach numbers, differences between Earth’s (primarily O2 and N2) and Mars’

(primarily CO2) atmosphere are thought to be negligible. That said, it is expected that the

100-fold change in density will completely offset the comparatively small change in viscosity,

specific heat ratio, and gas constant due to the change of gas type. Because of the high cost to

evacuate the PAL, the majority of the PAL testing is done in conjunction with other NASA

Ames projects already requiring vacuum; in doing so, the windows of time allotted to PAL

vacuum testing are often based on dual-use opportunities. Although not pursued for this project,

vacuum testing can be dedicated to the PAL if sufficient funding is in place, allowing for

extensive low-pressure testing. The PAL is shown in Figure 1.

Martian Surface Wind Tunnel

The Martian Surface Wind Tunnel (MARSWIT), shown in Figure 2, was first put into operation

in 1976 and is an open-circuit 43-foot-long atmospheric boundary-layer wind tunnel. The

3

internal cross section is 3.3 feet high by 4 feet wide [5]. As the MARSWIT is in the PAL near-

vacuum chamber, the wind tunnel can be tested at all atmospheric conditions of which the

facility is capable; at 1 atmosphere the wind tunnel can reach wind speeds of 34.5 ft/s, and at

5 millibars, wind speeds of 328 ft/s. The tunnel has been used to investigate the physics of

particle entrainment under Martian conditions, to test spacecraft instruments under Martian

conditions [5], and recently to test rotor performance. All test data presented in this paper was

acquired with the wind tunnel drive system turned off.

Figure 1. Planetary Aeolian Laboratory (PAL).

Figure 2. PAL Martian Surface Wind Tunnel.

4

TEST INSTALLATION, HARDWARE, AND DATA COLLECTION

Hardware Installation

Test hardware was installed into the MARSWIT test section, approximately located midway

along the 43-foot-long wind tunnel. Testing consisted of both two-bladed and four-bladed rotor

configurations. The two-bladed rotor was used to test a rotor in nominal helicopter mode. The

four-bladed rotor resembled the MH’s coaxial design, and provided increased rotor thrust

representative of the MH design. However, unlike the MH’s coaxial system, both rotors in the

four-bladed configuration are fixed, rotating in the same direction, at 90-degree orientation. Both

the two- and four-bladed rotor configurations are shown in Figure 3.

Test hardware was designed such that the rotor could be tested between ±14 degrees angle of

attack. For the presented data, all tests were conducted at –14 degrees, pitching the test apparatus

towards the tunnel inlet. Figure 4 shows the two-bladed rotor configuration at 0 and –14 degrees

(forward flight). Figure 5 shows the rotor again at –14 degrees, but from downstream of the test

section.

Figure 3. Left and right images show two- and four-bladed rotor configurations tested in the

MARSWIT test section, respectively.

Figure 4. Left image shows two-bladed rotor at a 0-degree shaft angle; right image shows

two-bladed rotor at a –14-degree shaft angle.

5

Figure 5. Two-bladed rotor at a –14-degree shaft angle, looking downstream of the test section.

Testing was conducted from a pressure range of 1 atmosphere (Earth’s atmosphere) down to

5.5 millibars (conditions which approximate the atmospheric conditions found on Mars).

Test Hardware

The primary goals were to collect rotor thrust, RPM, power, torque, motor temperature, and wind

speed, as well as chamber pressure, humidity, and temperature, while in forward flight. The

following sections discuss the hardware and sensors used to obtain this data, and reference

Figure 6 and Figure 7 for location within the MARSWIT.

Figure 6. Side profile of the 43-foot-long MARSWIT.

Vm

6

Figure 7. Hardware and sensor installation within the MARSWIT test section.

Prior to MH testing in the JPL 25-foot Space Simulator, a 1-atmosphere rotor hover safety

checkout needed to be conducted within the chamber. As part of this effort, the 40x22 rotor was

selected in 2015 and tested for this activity [6]. The same rotor blades and motor were used for

reduced pressure forward flight testing at NASA Ames Research Center in 2017.

To provide a better understanding of what the MH might experience during forward flight on

Mars, the selected rotor was chosen based on the physical dimensions and operating conditions

of the MH. The projected MH will be equipped with a coaxial rotor system, with rotor disks

approximately 3.94 feet in diameter. However, because of restrictions in MARSWIT test section

dimensions, the largest testable rotor was limited to 3.33 feet in diameter, approximately

0.65 feet smaller than what will be installed on the MH. In addition to rotor diameter, the

selected rotor was chosen to be operational up to 3000 RPM to match the RPM and hover tip

Mach Number of the proposed MH.

The selected rotor is highly twisted and defined by the manufacturer as 40x22. The first number

represents the rotor diameter in inches. The second number refers to the forward distance

traversed, in inches, for every rotor revolution when acting as a propeller [7].

The Siemens Electric AC Motor, model #1FT5104-0AF71-I, was used for rotor operation. This

motor was selected for the first-ever Martian atmosphere rotor hover testing in 2002, which also

took place in the PAL near-vacuum chamber [8]. Because this motor was proven to successfully

operate extensively under vacuum, it was chosen again for this test. Measurements included

RPM based on a motor encoder and torque based on motor current; both RPM and torque were

Infrared Sensor

Load cell (3)

Accelerometer (2) Actuator

Motor

Thermocouple

Potentiometer

18

Experim ent: H ardw are an d Senso rs

Infrared Sensor

Accelerom eter (2)

Actuator

Potentiom eter

Therm ocouple

M otor

Load cell (3)

7

recorded by the Data Acquisition System (DAS). A thermocouple was mounted to the motor for

motor temperature monitoring.

An Omron #E3S-AR11 infrared (IR) sensor was used during testing. This is a built-in amplifier

photoelectric feedback sensor, which was used to indicate motor RPM. Reflective tape, adhered

to the motor shaft, reflects the IR signal once per motor revolution. This sensor was only used to

monitor RPM while testing and was not recorded.

To measure rotor thrust, the motor is fixed to three Sensortronics S-Beam load cells, model

#60001. Each load cell is single axis and can measure up to 50 pounds within a safe margin. The

collective 150-pound measurable weight is required to accommodate the dead weight of the

motor and rotor hardware. The load cells were mounted 120 degrees apart about the rotor’s axis

of rotation.

At 1 atmosphere, rotor thrust is much larger than that at reduced pressure. As the PAL is

evacuated to Martian pressures, the atmospheric density within the chamber is approximately

100 times lower than at 1 atmosphere. Consequently, the load cells are operating at their

minimum specifications when measuring thrust at extremely low chamber pressures.

MARSWIT wind speed is determined from a 1-millibar (Barocel-590) and a ±1.25-millibar

(Setra 239) differential pressure transducer attached to a pitot-static probe, located forward of the

test section. The transducer, a model Barocell-590, was on a heated plate located in the PAL

control room to minimize temperature drift and was only used for 1-atmosphere measurements.

Wind speed is measured only in the direction of air entering the MARSWIT inlet. Moreover,

when the atmospheric pressures were different from 1 atmosphere, wind speed was only

collected for the two-bladed rotor.

To determine the test hardware structural resonance, a resonant frequency test was performed for

each rotor configuration. Within the maximum testable range of 3400 RPM, frequencies with

the highest amplitude occur around 1900 RPM for both the two- and four-bladed rotor

configurations.

Vibrations were monitored throughout testing by two uniaxial 5g Kistler accelerometers

mounted 90 degrees of relative rotation between each other, on a plane perpendicular to the axis

of rotation. Accelerometer installation was for the sole purpose of monitoring amplitude

throughout testing, particularly around determined resonant frequencies.

Acoustics measurements (not presented in this paper) were taken by microphones placed in the

vacuum chamber. The microphones and amplifiers are part of a G.R.A.S. Sound & Vibration

System.

Absolute chamber pressure, density, humidity, and temperature sensors located in the PAL

vacuum chamber were used for this test. The Setra 204 absolute pressure transducer was used to

measure chamber pressure for pressures ranging from 1 atmosphere to around 5.5 millibars. In

addition, the Wallace and Tiernan FA129 absolute pressure gauge was used just to indicate

absolute pressures of the same range as the Setra 204. One MKS Baratron 127AA 0–13-millibar

8

absolute pressure transducer was used when low pressures were reached. Lastly, humidity and

temperature were measured by a Vaisala DMP248 dewpoint transmitter.

Data Collection

All sensor cables bridge the vacuum chamber wall to the PAL control room, where they are

recorded to one of two data systems, an AstroMed Dash 18X (AstroMed) and a PAL LabVIEW

system. The AstroMed is a 14-bit DAS used for real-time monitoring and data recording, with

real-time sensor calibration and filter application. Rotor thrust, RPM, power, torque, wind speed,

acoustics, and stand vibration were recorded to this system. The PAL LabVIEW system recorded

absolute chamber pressure, density, humidity, and temperature. In addition to the PAL digital

readout of chamber pressure, pressure was also manually recorded from the Wallace and Tiernan

FA129 absolute pressure gauge.

POST-PROCESSING

Post-processed data records are merged based on the time stamp of each DAS described prior.

Once merged, the data undergoes zero-point subtraction of load cell weight and torque. Periodic

zero-point subtraction became particularly important when measuring rotor thrust, as the three

load cells demonstrated drift during extended operation; routine zero-points helped capture and

mitigate this behavior. In addition to zero-point subtraction, a rotor hub torque tare was applied.

Data Acquisition

There were three data acquisition sources used during the test: an Astro-Med Dash-18 was used

to acquire measurements of model instrumentation; an N242 facility data system was used to

acquire facility measurements; and a manually recorded run log was used to record model

configuration and select facility measurement values, as well as notes about recorded points

when needed. The Astro-Med Dash-18 internally processes the acquired data signals to save data

in engineering units rather than as voltages, while the N242 facility data system contains both

files in engineering units and voltages.

The Astro-Med Dash-18 was set to record channels simultaneously at two different sampling

rates, a standard and slow rate. The standard rate was either 200 Hz or 100,000 Hz, and the slow

rate was either 100 Hz or 200 Hz, respectively. The 100,000-Hz rate was used to support

acoustic measurements. The N242 resident data system recorded data at approximately 3 Hz.

The N242 facility data system and the Astro-Med Dash-18 were independent systems with

independent operators. The only synchronization between the systems was that the operators

would initiate dataset recording at the same time based on a verbal cue. Data file names for the

two systems were also independent, so correlation between data sets was determined by log

records of the initial and ending N242 dataset file names in a run and by comparing time stamps

of the dataset files from both systems. Although the N242 resident data system was always

operational for monitoring facility conditions, datasets were not always acquired for each record

point acquired by the Astro-Med Dash-18. For record points missing an N242 dataset, the run

log was used to provide tunnel conditions.

9

Data was acquired for a predetermined series of runs with points for specific model and facility

settings. However, since tests always have run-time issues, some of the points had to be repeated

and some additional data record points were acquired that did not have point numbers assigned.

To allow for easy identification of individual point datasets, each dataset was assigned a unique

run and sequence number pair. The run number was same as specified in the run log, but the

sequence numbers were based on the ordinal sequence in which the point datasets were acquired.

For clarity, the final run and sequence numbers presented in this report have been renumbered.

Initial Post-Processing

The datasets acquired from the N242 facility data system and the Astro-Med Dash-18 contain

time histories of their measurement channels. The first step in post-processing is to read all of the

time history datasets from both systems and create summary databases where each row contains

the means and standard deviations for each channel; a file name of the point dataset and its time

stamp for each data point follow next. The information from the run logs is read in from Excel

spreadsheets created for each log and used to create a single, combined log table. A log

configuration file is used in this process to resolve formatting and column name differences

between the individual logs.

Run and point numbers are used to match log data and Astro-Med Dash-18 data. The N242

facility data system uses a different numbering scheme, so time stamps are used to match N242

system points with Astro-Med points. A dry run is performed to sync the three databases to

determine if there are problems that need to be corrected. The most common problem is

inconsistencies in the logs, which are managed by editing the logs to resolve them. Only data

means and standard deviations are included in the merged database.

Zero Corrections

Zero record points were taken before and after each run and RPM sweep. Moreover, to further

counteract temperature and recirculation effects, there are sets of runs in which, in addition to

taking a zero before and after each RPM sweep, a zero point was taken in between each RPM

measurement.

The purpose of a “zero” record point is to determine the change in measurement values from

values obtained at a reference condition, which is currently defined as zero tunnel wind speed

and zero rotor RPM. For selected measurements, the zero value is subtracted from all

measurements obtained during the run in which the zero was recorded and for subsequent runs if

no new zeros were obtained. Three types of zero corrections are used depending on the

availability of zero and static points: “beginning” zero corrections in which the values for a

zero/static point are subtracted from subsequent points, “ending” zero corrections in which the

values for a zero/static point are subtracted from previous points, and “both” zero corrections in

which the interpolated values from beginning and ending zero/static points are subtracted from

points taken in between. The interpolation is based the data point record time.

10

Weight Tares

Weight tares are the changes in loads measured by loads cells due to shifting weight of the model

as the angle is changed in the absence of aerodynamic forces. Measurements of these tares, after

zero corrections were made, are presented in Figure 8. As expected, the number of props

installed does make a small difference on the magnitude tare loads. Load cell 3 is located on the

pivot axis (see Figure 12), resulting in somewhat higher noise levels. The load cell force

measurement has estimated tare force subtracted after the zero corrections are applied. The tare

estimates are made using the fit equation: Tare = S1∗(1.0−cos(α) + S2∗sin(α). The coefficients

for the load cell curve fits and the fit standard deviations are presented in Table 1.

Figure 8. Weight tare values for load cells 1, 2, and 3.

Table 1. Weight tare fit coefficients with standard deviations.

Nprops Load Cell S1 S2 Sigma (lb)

0 1 11.99386754 –40.13675701 0.358695099

0 2 27.11330234 37.90820162 0.131569142

0 3 33.50985781 –6.215704452 0.318109694

1 1 17.06010815 –39.7085289 0.403321397

1 2 65.84885034 40.32774456 0.441892038

1 3 0 –5.495353688 0.333470585

2 1 10.07770625 –40.08493139 0.339950515

2 2 41.14243824 38.40839435 0.300244256

2 3 22.76007772 –5.412475948 0.319728605

11

This weight tare fit is not applied when the angle of the zero record point is the same as the point

being analyzed. All data presented in this report was collected at an angle of –14 degrees.

Therefore, this weight tare fit is not applied to the presented data.

Aerodynamic Tares

Corrections for aerodynamic tares were considered. These were forces on the model that occur

with positive wind speed and no props installed. Two characteristics were expected: first, that the

tares should be proportional to dynamic pressure, and second, that the tare forces should have

some symmetry about the 0-degree tilt angle. Neither of these expectations seemed evident in the

data, so it may be that the tare forces were masked by data scatter. It was therefore decided not to

calculate and apply aerodynamic tares at this time.

Torque Tares

After zero corrections and weight tare corrections, torque tares were considered. The torque

required to spin the motor with no propellers installed was monitored throughout the RPM range

and for 1 atmosphere and reduced pressures. As an improvement to the previous data report [1],

an improved torque tare was applied to the experimental data herein.

In addition, at 1-atmosphere data collection, points were collected to up to 200 millibars when

the propellers were spinning and the pressure changed at a rate of less than 1 millibar per minute.

Further, when the rotors were at reduced pressures, they were spun at higher RPMs than when

they were at 1 atmosphere. Therefore, two sets of torque tares (see Figure 9 and Figure 10) were

created to cover the range of tested RPM at 1 atmosphere and at reduced pressures.

Absolute Pressure Offset Correction

The Setra 204 was used to record absolute pressure from 1 atmosphere down to 5.5 millibars,

and this measurement is part of the recorded data in the N242 system. It was identified that this

measurement required a correction in the offset of its calibration. Since this setting could not be

directly changed in the N242 system, this offset was instead corrected in the data post-

processing.

A Mensor CPC6000 automated pressure calibrator [9] was used to find the corresponding offset.

The automated pressure calibrator was connected to the Setra 204, and multiple points were

collected ranging from 1 atmosphere to reduced testing pressures comparable to those seen in

testing. The difference between the Setra 204 and the automated pressure calibrator readings was

fairly constant within this range (see Table 2 and Figure 11). Therefore, the average of all of

these readings was calculated and subtracted from the Setra 204 readings.

12

Figure 9. Torque tares at reduced pressures.

Figure 10. Torque tares at 1 atmosphere.

13

Table 2. Readings of automated pressure calibrator vs. Setra 204.

Automated Pressure Calibrator (mbar)

Setra 204 (mbar) Offset (mbar)

11.990 18.666 6.676

12.000 18.658 6.658

14.050 20.773 6.723

14.060 20.781 6.721

20.020 26.774 6.754

20.020 26.779 6.759

29.990 36.731 6.741

40.000 46.687 6.687

60.000 66.627 6.627

100.300 106.903 6.603

100.450 107.033 6.583

200.000 206.583 6.583

303.000 309.553 6.553

404.900 411.573 6.673

404.990 411.615 6.625

606.690 613.452 6.762

606.720 613.482 6.762

699.800 706.526 6.726

749.990 756.656 6.666

800.220 806.813 6.593

801.210 807.837 6.627

850.150 856.648 6.498

899.730 906.088 6.358

997.650 1004.269 6.619

1021.020 1027.692 6.672

Average: 6.650

Figure 11. Setra 204 offset vs. pressure.

1

2

3

4

5

6

7

8

9

10

0 100 200 300 400 500 600 700 800 900 1000

Off

set

(mb

ar)

Setra 204 Pressure (mbar)

Setra 204 Offset

Offset

Linear (Offset)

14

Force and Moment Calculations

The helicopter test apparatus is mounted on three vertically oriented load cells, positioned as

shown in Figure 12. The bolt holes for the load cells are on a circle with a radius of 5.455 inches,

that is normal to and centered along the rotor’s shaft axis. The load cells are mounted below the

model and remain perpendicular to the shaft axis as the model is rotated in pitch. Negative shaft

angle is defined as tilting the shaft into the wind.

The load cells read positive in tension, which is confirmed by the recorded weight tares that

show load cell #1 having a more positive reading when the pitch is at –14 degrees (tilted into the

wind) and load cell #2 having a more negative reading at that pitch angle (see Figure 8). It

should be noted that moment values include contributions from side force and drag due to their

application occurring at a point several inches above the load cells. It is not possible to remove

these contributions since there are no measurements of side force or drag.

Rotor Configurations

Figure 13 shows the rotor in nominal forward flight, thrusting-up configuration. All sign

conventions are the same for both configurations, except for torque, which is positive for all

positive RPMs.

The presented sign conventions and definitions are in association with a rotor thrusting up and

can be applied to all data presented in this report. The angle of attack of the rotor disk, or

equivalently, the geometric shaft angle, is defined such that the rotor disk is at 0 degrees when

horizontal. When the front of the disk (facing upstream) pitches upwards, the angle of attack is

increased, effectively pointing the thrust vector more downstream. All data presented in this

report was performed at –14 degrees geometric shaft angle, so the thrust vector points partially

upstream. The positive axis directions and resulting positive moment directions are illustrated in

Figure 13.

Figure 12. Load cell locations. Bolt holes are on a radius of 5.455 inches.

15

Figure 13. Rotor thrusting up in forward flight, view from ceiling.

Azimuth angle of thrust vector location, , is obtained by calculating the angle between the Mx

and My components, measured counterclockwise from 0-degree azimuth.

Drag and Side Force Contributions to Measured Moments

The load cells are aligned with the rotor shaft, so in the body-axis system they measure thrust,

but no component of either drag or side force. However, drag will contribute to measured pitch

moments, My, and side force will contribute to measured roll moments, Mx. Since there are no

measurements of drag and side force, their contributions to pitch and roll moments can only be

estimated using analytic or computational predictions of drag and side force. The rotor in

nominal forward flight is shown in Figure 14 with the drag force vector shown in the body axis

system. This shows that the contribution to pitching moment, My, due to drag is D * ZD, where

D is the magnitude of the drag and ZD is the moment arm, along the z-axis, from where drag is

applied to the centers of the load cells. In a similar manner, side force, S, contributes to the

measured rolling moment, Mx. Note that model weight makes no contributions if the data is

corrected for zeros and weight tares.

Figure 14. Drag contribution to pitching moment, body-axis system.

x

z

Drag @ zD

16

PRESENTED DATA

Both two- and four-bladed rotor configurations were tested over a pressure range of 1 bar down

to 5 millibars, up to 3400 RPM, and at a fixed forward flight shaft angle of –14 degrees.

Atmospheric conditions expected on Mars during the daytime include densities ranging from

0.00087 to 0.00125 lb/ft3

[10], which are the densities in which the MH is designed to operate

[11]. Therefore, pressure was held at values that caused chamber density to be close to the

aforementioned range. In addition, the rotors were tested over a pressure range to analyze

Reynolds number effect on rotor performance.

Runs 1 to 7 and 37 to 86 incorporated the four-bladed rotor configuration, and runs 8 to 36

incorporated the two-bladed rotor configuration. Table 3 below outlines the categories data can

be broken into.

Pressure Decrease

The PAL can evacuate from 1 bar to 5.5 millibars in approximately 45 minutes. Most of the data

in this condition was taken without the rotor spinning. However, there was one run in which the

two-bladed rotor was run from 2000 to 3400 RPM from 70 to 10 millibars to investigate the flow

in the wind tunnel under this condition. The RPM chosen depends on two things. First, it was

chosen to avoid test stand resonance determined through Resonance Assessment Profile (RAP)

testing. Second, as rotor thrust and vibration is greatest at 1 bar, monitoring of accelerometer and

load cell readings limited maximum RPM for safe MARSWIT testing. Table 4 specifies the rotor

test conditions.

Table 3. Executed test matrix.

Chamber Test Condition Test Approach

Pressure Decrease

Pressure decrease from 1 bar down to 5.5 millibars, constant –14-degree rotor shaft angle, wind off, and rotor not spinning. Within this condition there is one run exception where the two-bladed rotor was run from 2000 to 3400 RPM from 70 to 10 millibars.

Constant Pressure

Data in this condition is collected at 1 atmosphere and also when pressure was held at pressures close to the range of expected Martian atmospheric densities during daytime (0.00087 to 0.00125 lb/ft

3 [10]). Data is taken from 0 rotor RPM up to 2100 and 3400

RPM for terrestrial and Mars-like conditions, respectively. Constant –14-degree rotor shaft angle, wind off.

Pressure Drift Pressure drift at 1 millibar per minute, from 5.5 to 200 millibars, rotor RPM from 0 to 3400 RPM, constant –14-degree rotor shaft angle, wind off.

Pressure Increase Pressure increase from approximately 200 millibars up to 1 bar, constant RPM, constant –14-degree rotor shaft angle, wind off.

17

Constant Pressure

Constant pressure can occur at 1 atmosphere and when pressure is held at Mars-like conditions.

To decrease pressure, the valve connecting the SVS to the PAL has to be opened. That said,

holding constant pressure is currently a challenge in the facility. When reduced pressures are

reached, and the PAL is closed off from the SVS, the facility leaks at a rate of roughly 1 millibar

per minute. Thus, to hold constant pressure, the facility operator manually regulates the opening

of the valve until the desired pressure is steady. However, once manual regulation of the valve

ceases, the pressure can deviate up to 5 percent from the steady pressure reached in some

instances. Currently, there is no automatic device controlling the valve that can rapidly account

for the loss of pressure and set the valve to a desired position without continuous variation.

Two different runs where taken under this condition; a zero RPM point was collected before and

after each RPM sweep, and a zero RPM point was taken in between each RPM point. Table 5

shows the range of tested RPM for the two- and four-bladed rotor.

Pressure Drift

If vacuum to the PAL is shut off by the SVS, pressure within the PAL will slowly drift at a rate

of 1 millibar per minute. To provide ample data points while minimizing the amount of pressure

drift, 15-second data record lengths were collected. As PAL pressure evacuation is dependent on

the number of other NASA Ames facilities requiring vacuum, the pressure in which SVS

disconnects the PAL from vacuum varied throughout the test program. Reynolds number effects

on rotor performance were investigated during this pressure drift condition. Table 6 shows the

range of tested RPM and the test conditions for the two- and four-bladed rotor.

Table 4. Test RPMs for each configuration as PAL pressure was evacuated. The exact

pressure the chamber was evacuated to varied throughout testing.

Rotor Configuration Pressure (millibars) RPM

Four-bladed ~1000 down to 5.5 0

Two-bladed ~1000 down to 10 0 to 3400

Table 5. Range of tested RPM for two- and four-bladed rotors as pressure was held in

the vacuum chamber.

Rotor Configuration Target Pressure (millibars) RPM

Two-bladed ~1000 0 to 2100

Four-bladed ~1000 0 to 2000

Two-bladed 11 0 to 3400

Four-bladed 14 0 to 3400

Table 6. Range of tested RPM for each configuration.

Rotor Configuration Pressure (millibars) RPM

Two-bladed 11 to 200 0 to 3400

Four-bladed 5.5 to 200 0 to 3400

18

Table 7. RPM for the four-bladed configuration, as PAL pressure was evacuated.

Rotor Configuration Pressure (millibars) RPM

Four-bladed 200 to 1000 1250

Pressure Increase

As pressure was increased, the rotors were not spinning for most of the runs. However, there was

one run in which the four-bladed rotor was set to a constant RPM while the pressure increased.

Table 7 shows the RPM and the test conditions for the four-bladed rotor.

CONCLUSIONS

Despite the challenges involved in testing at the large difference of atmospheric densities

between Earth and Mars, successful rotor testing operations measuring thrust, torque, power, and

wind speed were demonstrated in the MARSWIT at Martian atmospheric densities and low

speeds. Forward flight rotor performance was measured for a two- and four-bladed rotor at

terrestrial and Martian atmospheric density conditions. In addition, Reynolds number effects on

rotor performance were analyzed for pressures ranging from 40 to 200 millibars. Repeatability at

Mars-like conditions was demonstrated with the two-bladed rotor for thrust, torque, power, and

wind speed measurements, where differences between the results exhibited an average of no

more than 5 percent. In addition to rotor behavior, rotor-induced wind tunnel velocity was

compared from Martian atmospheric densities against results at 1 atmosphere.

Analysis of Reynolds number effects on rotor performance for both rotor configurations made

from 2x104 to 9x10

4 showed that CT and FM decreased around 26 and 36 percent, respectively.

Further, CT and FM exhibited roughly a second-degree polynomial trend for both rotor

configurations when plotted against Re0.75R within this range of Re. Moreover, CP remained

fairly constant, exhibiting variations of no more than 5.5 percent.

FUTURE WORK Wind Tunnel Construction

A larger low-pressure wind tunnel is currently under construction and will be placed alongside

the MARSWIT in the PAL near-vacuum chamber. The new wind tunnel will have an 80-inch

cross section, which will decrease tunnel effects when testing rotors approximately 4 feet in

diameter. Further, to counteract PAL wind recirculation while chamber pressure is pumping

down, additional flow treatment will be added at the wind tunnel inlet.

19

REFERENCES

[1] G. A. Ament, W. J. F. Koning, and B. N. Perez Perez: Isolated Rotor Forward Flight

Testing at Martian Atmospheric Density Data Report, NASA/CR–2018-219736, May

2019.

[2] D. Brown, J. Wendel, and D. C. Agle: Mars Helicopter to Fly on NASA’s Next Red Planet

Rover Mission. Available: https://www.nasa.gov/press-release/mars-helicopter-to-fly-on-

nasa-s-next-red-planet-rover-mission. Accessed: 13-Aug-2018.

[3] W. J. F. Koning, W. Johnson, and B. G. Allan: Generation of Mars Helicopter Rotor Model

for Comprehensive Analyses, in AHS Aeromechanics Design for Transformative Vertical

Flight, 2018.

[4] NASA - Planetary Aeolian Laboratory. Available: https://www.nasa.gov/centers/ames/

business/planetary_aeolian_facilities.html. Accessed: 03-Aug-2017.

[5] PAL | The Ronald Greeley Center for Planetary Studies. Available: https://rpif.asu.edu/

index.php/pal/. Accessed: 23-Nov-2017.

[6] M. McCoy, A. J. Wadcock, and L. A. Young: Documentation of the Recirculation in a

Closed-Chamber Rotor Hover Test, NASA TM-2016-219162, Aug. 2016.

[7] W. J. F. Koning: Generation of Performance Model for the Aeolian Wind Tunnel (AWT)

Rotor at Reduced Pressure, NASA CR-2018-219737, Jan. 2018.

[8] L. A. Young and E. W. Aiken: Engineering Studies into Vertical Lift Planetary Aerial

Vehicles, in AHS International Meeting on Advanced Rotorcraft Technology and Life

Saving Activities, Utsunomiya, Tochigi, Japan, 2002.

[9] CPC6000 Operating Instructions Modular Precision Pressure Controller Operating

Instructions-CPC6000, Mensor, 2016, p. 105.

[10] J. (Bob) Balaram et al.: Mars Helicopter Technology Demonstrator, AIAA Science and

Technology Forum and Exposition (AIAA SciTech), Kissimmee, FL, 2018.

[11] H. F. Grip et al.: Guidance and Control for a Mars Helicopter, AIAA Science and

Technology Forum and Exposition (AIAA SciTech), Kissimmee, FL, 2018.

20

APPENDIX A—ISOLATED ROTOR HARDWARE TECHNICAL DRAWINGS

21

22

23

24

25

26

27

28

29

30

31

32

33

34

APPENDIX B—CORRECTED DATA

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 1 1022.4 0 0 0 0 0

2 7.68E-02 61.3 0.02 0 0 0 1.57E-04

1 2 1022.4 602 4.81 0.13 -1.5 2.04E-02 -3.16E-04 0.73 6

2 7.68E-02 61.3 1.12 0.09 2.49 3.46E-03 5.26E-04 0.09 1.57E-04 121

1 3 1022.4 801 8.95 0.31 -3.49 2.15E-02 -4.17E-04 0.77 6.9

2 7.68E-02 61.3 2.02 0.24 3.98 3.55E-03 4.74E-04 0.13 1.57E-04 131.3

1 4 1022.4 1000 14.07 0.6 -5.69 2.17E-02 -4.36E-04 0.78 9.3

2 7.68E-02 61.3 3.14 0.47 6.25 3.53E-03 4.78E-04 0.16 1.57E-04 132.3

1 5 1022.4 1201 20.74 1.03 -7.36 2.21E-02 -3.90E-04 0.81 11.3

2 7.68E-02 61.3 4.51 0.84 10.52 3.51E-03 5.58E-04 0.19 1.57E-04 125

1 6 1022.4 1299 24.01 1.31 -7.78 2.19E-02 -3.52E-04 0.8 12

2 7.68E-02 61.3 5.28 1.04 12.2 3.52E-03 5.53E-04 0.2 1.57E-04 122.5

1 7 1022.4 1397 28.52 1.64 -8.76 2.25E-02 -3.43E-04 0.82 12.6

2 7.68E-02 61.3 6.15 1.35 15.32 3.55E-03 6.00E-04 0.22 1.57E-04 119.8

1 8 1022.4 1596 37.24 2.46 -10.85 2.25E-02 -3.26E-04 0.82 14.7

2 7.68E-02 61.3 8.09 2.01 20.66 3.57E-03 6.20E-04 0.25 1.57E-04 117.7

1 9 1022.4 1698 42.1 2.97 -12.47 2.25E-02 -3.31E-04 0.81 15.4

2 7.68E-02 61.3 9.2 2.42 23.43 3.59E-03 6.22E-04 0.27 1.57E-04 118

1 10 1022.4 1797 47.55 3.54 -14.31 2.27E-02 -3.39E-04 0.82 16.2

2 7.68E-02 61.3 10.36 2.9 27 3.61E-03 6.39E-04 0.28 1.57E-04 117.9

1 11 1022.4 1994 58.18 4.85 -16.52 2.25E-02 -3.18E-04 0.81 18.3

2 7.68E-02 61.3 12.78 3.93 36.54 3.62E-03 7.03E-04 0.31 1.57E-04 114.3

1 12 1022.4 0 0 0 0 0

2 7.68E-02 61.3 0.01 0 0 0 1.57E-04

2 1 1011.3 0 0 0 0 0.00E+00 NA

2 7.53E-02 66 0.31 0 0 0 1.62E-04

2 2 1011.3 500 3.48 0.07 -1.18 2.18E-02 -3.68E-04 0.79 7.86E+04 4.5

2 7.53E-02 66.1 0.77 0.06 1.66 3.53E-03 5.19E-04 0.08 1.62E-04 125.4

2 3 1017.9 1004 14.08 0.6 -4.72 2.18E-02 -3.62E-04 0.78 1.59E+05 9

2 7.58E-02 66 3.15 0.47 7.07 3.56E-03 5.43E-04 0.16 1.61E-04 123.7

35

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 4 1011.3 1004 13.95 0.6 -5.2 2.17E-02 -4.02E-04 0.78 1.58E+05 9.3

2 7.53E-02 66.1 3.13 0.47 7.51 3.56E-03 5.81E-04 0.16 1.62E-04 124.7

2 5 1011.3 1251 21.62 1.15 -6.91 2.17E-02 -3.45E-04 0.78 1.97E+05 11.4

2 7.53E-02 66.1 4.83 0.9 12.01 3.55E-03 5.99E-04 0.2 1.62E-04 119.9

2 6 1011.3 0 0 0 0 0.00E+00 NA

2 7.53E-02 66.1 0.34 0 0 0 1.62E-04

3 1 125.3 0 0 0 0 0.00E+00 NA

2 9.44E-03 60.1 0.27 0 0 0 1.29E-03

3 2 128.4 2984 15.55 2.36 -1.55 2.14E-02 -1.06E-04 0.65 6.01E+04 NA

2 9.66E-03 60.5 4.15 1.53 8.52 4.17E-03 5.82E-04 0.47 1.26E-03 100.3

3 3 128.8 2984 15.63 2.34 -3.01 2.14E-02 -2.05E-04 0.66 6.03E+04 NA

2 9.69E-03 60.6 4.12 1.54 7.66 4.13E-03 5.22E-04 0.47 1.26E-03 111.5

3 4 129.3 2984 15.64 2.32 -3.14 2.13E-02 -2.13E-04 0.66 6.05E+04 NA

2 9.73E-03 60.6 4.08 1.54 6.52 4.07E-03 4.42E-04 0.47 1.26E-03 115.8

3 5 130 2984 15.9 2.34 -4.47 2.16E-02 -3.01E-04 0.67 6.08E+04 NA

2 9.78E-03 60.7 4.12 1.57 6.28 4.09E-03 4.24E-04 0.47 1.25E-03 125.4

3 6 130.5 2984 15.86 2.32 -4.95 2.14E-02 -3.32E-04 0.67 6.11E+04 NA

2 9.82E-03 60.7 4.09 1.56 6.82 4.04E-03 4.58E-04 0.47 1.24E-03 125.9

3 7 131.1 2984 15.86 2.21 -3.8 2.14E-02 -2.55E-04 0.71 6.13E+04 NA

2 9.86E-03 60.8 3.89 1.56 6.15 3.83E-03 4.12E-04 0.47 1.24E-03 121.7

3 8 131.6 2984 15.93 2.21 -4.33 2.14E-02 -2.89E-04 0.71 6.15E+04 NA

2 9.90E-03 60.8 3.9 1.57 7.08 3.82E-03 4.72E-04 0.47 1.23E-03 121.5

3 9 132 2984 16.06 2.23 -3.94 2.15E-02 -2.62E-04 0.71 6.17E+04 NA

2 9.93E-03 60.9 3.92 1.58 7.2 3.83E-03 4.78E-04 0.47 1.23E-03 118.7

3 10 132.7 2984 16.06 2.22 -3.86 2.14E-02 -2.55E-04 0.71 6.20E+04 NA

2 9.98E-03 60.9 3.91 1.58 7.68 3.81E-03 5.08E-04 0.47 1.22E-03 116.6

3 11 133.3 2984 16.07 2.25 -3.26 2.13E-02 -2.14E-04 0.7 6.23E+04 NA

2 1.00E-02 61 3.96 1.58 7.25 3.83E-03 4.77E-04 0.47 1.22E-03 114.2

3 12 133.9 2984 16.35 2.28 -4.52 2.16E-02 -2.97E-04 0.71 6.26E+04 NA

2 1.01E-02 61 4.01 1.62 7.27 3.87E-03 4.77E-04 0.47 1.21E-03 121.9

3 13 134.7 2984 16.29 2.26 -3.96 2.14E-02 -2.58E-04 0.71 6.29E+04 NA

2 1.01E-02 61.1 3.98 1.6 8.22 3.81E-03 5.36E-04 0.47 1.21E-03 115.7

36

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

3 14 135.3 2984 16.52 2.28 -4.25 2.16E-02 -2.76E-04 0.72 6.32E+04 NA

2 1.02E-02 61.1 4.02 1.63 7.77 3.84E-03 5.04E-04 0.47 1.20E-03 118.7

3 15 136 2984 16.42 2.28 -3.17 2.13E-02 -2.05E-04 0.71 6.35E+04 NA

2 1.02E-02 61.2 4.01 1.62 8.36 3.81E-03 5.40E-04 0.47 1.20E-03 110.8

3 16 136.4 2984 16.45 2.28 -3.91 2.13E-02 -2.52E-04 0.71 6.37E+04 NA

2 1.03E-02 61.3 4.02 1.62 7.98 3.81E-03 5.13E-04 0.47 1.19E-03 116.1

3 17 137.1 2984 16.56 2.3 -3.55 2.14E-02 -2.27E-04 0.71 6.40E+04 NA

2 1.03E-02 61.3 4.05 1.63 8.48 3.82E-03 5.43E-04 0.47 1.19E-03 112.7

3 18 137.7 2984 16.61 2.31 -2.76 2.13E-02 -1.76E-04 0.71 6.43E+04 NA

2 1.03E-02 61.4 4.07 1.63 7.06 3.82E-03 4.50E-04 0.47 1.18E-03 111.4

3 19 139.3 2984 16.75 2.35 -2.91 2.13E-02 -1.84E-04 0.7 6.50E+04 NA

2 1.05E-02 61.5 4.13 1.64 7.01 3.83E-03 4.42E-04 0.47 1.17E-03 112.6

3 20 139.9 2984 16.85 2.36 -3.7 2.13E-02 -2.33E-04 0.7 6.53E+04 NA

2 1.05E-02 61.6 4.15 1.66 9.4 3.83E-03 5.90E-04 0.47 1.16E-03 111.5

3 21 140.4 2984 16.91 2.37 -3.71 2.13E-02 -2.32E-04 0.7 6.55E+04 NA

2 1.05E-02 61.6 4.18 1.66 8.11 3.85E-03 5.08E-04 0.47 1.16E-03 114.6

3 22 141.3 2984 17 2.38 -4.54 2.13E-02 -2.83E-04 0.7 6.59E+04 NA

2 1.06E-02 61.7 4.18 1.67 8.82 3.83E-03 5.49E-04 0.47 1.15E-03 117.3

3 23 141.7 2984 17.05 2.38 -3.45 2.13E-02 -2.14E-04 0.7 6.61E+04 NA

2 1.06E-02 61.7 4.19 1.68 9.31 3.83E-03 5.77E-04 0.47 1.15E-03 110.4

3 24 142.2 2983 16.95 2.39 -1.95 2.11E-02 -1.21E-04 0.69 6.63E+04 NA

2 1.07E-02 61.8 4.21 1.66 8.94 3.83E-03 5.53E-04 0.47 1.15E-03 102.3

3 25 142.6 2984 17.02 2.39 -4.06 2.11E-02 -2.50E-04 0.7 6.64E+04 NA

2 1.07E-02 61.8 4.21 1.67 8.69 3.82E-03 5.36E-04 0.47 1.14E-03 115

3 26 142.9 2983 16.95 2.39 -4.04 2.10E-02 -2.49E-04 0.69 6.66E+04 NA

2 1.07E-02 61.8 4.21 1.65 8.4 3.81E-03 5.17E-04 0.47 1.14E-03 115.7

3 27 143.5 2983 17.1 2.41 -4.25 2.11E-02 -2.60E-04 0.69 6.69E+04 NA

2 1.08E-02 61.9 4.25 1.67 9.02 3.83E-03 5.53E-04 0.47 1.14E-03 115.2

3 28 143.9 2983 17.17 2.41 -4.34 2.11E-02 -2.65E-04 0.7 6.70E+04 NA

2 1.08E-02 61.9 4.25 1.68 10.12 3.82E-03 6.18E-04 0.47 1.13E-03 113.2

3 29 144.3 2983 17.14 2.44 -2.27 2.10E-02 -1.38E-04 0.69 6.72E+04 NA

2 1.08E-02 62 4.29 1.67 7.75 3.85E-03 4.72E-04 0.47 1.13E-03 106.3

3 30 144.7 2983 17.31 2.44 -5 2.12E-02 -3.04E-04 0.7 6.74E+04 NA 37

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 1.09E-02 62 4.29 1.7 9.23 3.84E-03 5.61E-04 0.47 1.13E-03 118.4

3 31 145 2983 17.36 2.44 -4.28 2.12E-02 -2.60E-04 0.7 6.75E+04 NA

2 1.09E-02 62 4.29 1.7 10.26 3.83E-03 6.23E-04 0.47 1.12E-03 112.6

3 32 145.5 2983 17.24 2.45 -3.49 2.10E-02 -2.11E-04 0.69 6.77E+04 NA

2 1.09E-02 62.1 4.31 1.68 7.99 3.83E-03 4.83E-04 0.47 1.12E-03 113.6

3 33 71.4 0 0 0 0 0.00E+00 NA

2 5.38E-03 60.1 -0.01 0 0 0 2.27E-03

4 1 13.4 0 -0.12 0 0.08 0.00E+00 NA

2 1.01E-03 59.4 0.23 0 0.14 0 1.24E-02 -119.2

4 2 13.3 1993 -0.05 0.08 1.41 -1.53E-03 2.08E-03 -0.01 4.08E+03 NA

2 1.01E-03 59.5 0.22 0 -0.56 4.81E-03 -8.23E-04 0.31 1.25E-02 158.4

4 3 13.6 2091 0.27 0.09 0.81 7.07E-03 1.06E-03 0.11 4.38E+03 NA

2 1.03E-03 59.6 0.24 0.01 -0.16 4.54E-03 -2.15E-04 0.33 1.22E-02 -11.5

4 4 13.7 2091 0.3 0.09 0.66 7.76E-03 8.63E-04 0.13 4.38E+03 NA

2 1.03E-03 59.7 0.24 0.01 -0.16 4.52E-03 -2.11E-04 0.33 1.22E-02 -13.8

4 5 13.4 2197 0.42 0.1 0.38 1.02E-02 4.64E-04 0.21 4.51E+03 NA

2 1.01E-03 60 0.24 0.02 -0.38 4.17E-03 -4.52E-04 0.35 1.24E-02 -44.3

4 6 14.4 2293 0.45 0.11 0.73 9.20E-03 7.50E-04 0.2 5.08E+03 NA

2 1.09E-03 60.4 0.26 0.02 -0.63 3.89E-03 -6.47E-04 0.36 1.15E-02 -40.8

4 7 15.5 2394 0.61 0.13 0.77 1.08E-02 6.78E-04 0.25 5.68E+03 NA

2 1.16E-03 60.5 0.29 0.03 -0.66 3.80E-03 -5.79E-04 0.38 1.07E-02 -40.5

4 8 15.9 2492 0.67 0.16 0.7 1.06E-02 5.53E-04 0.24 6.06E+03 NA

2 1.19E-03 60.5 0.33 0.04 -0.71 3.88E-03 -5.64E-04 0.39 1.05E-02 -45.5

4 9 16.3 2593 0.91 0.18 0.61 1.31E-02 4.33E-04 0.33 6.49E+03 NA

2 1.23E-03 60.6 0.37 0.06 -0.57 3.89E-03 -4.06E-04 0.41 1.02E-02 -43.2

4 10 16.7 2690 1.1 0.2 0.28 1.43E-02 1.78E-04 0.4 6.89E+03 NA

2 1.25E-03 60.6 0.39 0.08 -0.41 3.75E-03 -2.66E-04 0.42 9.94E-03 -56.2

4 11 17 2789 1.13 0.23 0.42 1.34E-02 2.47E-04 0.36 7.27E+03 NA

2 1.28E-03 60.6 0.43 0.08 -0.14 3.77E-03 -8.42E-05 0.44 9.76E-03 -18.8

4 12 17.3 2888 1.27 0.26 0.56 1.38E-02 3.04E-04 0.37 7.69E+03 NA

2 1.30E-03 60.7 0.47 0.1 -0.02 3.77E-03 -1.18E-05 0.45 9.56E-03 -2.2

4 13 17.7 2988 1.37 0.3 0.71 1.36E-02 3.52E-04 0.36 8.11E+03 NA

38

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 1.33E-03 60.7 0.52 0.11 -0.03 3.81E-03 -1.28E-05 0.47 9.37E-03 -2.1

4 14 18.1 3084 1.56 0.34 0.91 1.43E-02 4.14E-04 0.38 8.58E+03 NA

2 1.36E-03 60.8 0.58 0.13 0.06 3.86E-03 2.51E-05 0.48 9.15E-03 3.5

4 15 17.9 3183 1.73 0.38 1.28 1.50E-02 5.51E-04 0.41 8.76E+03 NA

2 1.35E-03 60.9 0.62 0.15 -0.04 3.92E-03 -1.63E-05 0.5 9.25E-03 -1.7

4 16 17.5 3282 1.79 0.41 1.22 1.50E-02 5.05E-04 0.4 8.79E+03 NA

2 1.31E-03 60.9 0.65 0.16 -0.01 3.96E-03 -4.10E-06 0.52 9.50E-03 -0.5

4 17 17.1 3378 1.86 0.44 1.26 1.51E-02 5.04E-04 0.4 8.84E+03 NA

2 1.28E-03 60.9 0.68 0.17 0.16 4.03E-03 6.59E-05 0.53 9.73E-03 7.5

4 18 16.6 0 0 0 0 0.00E+00 NA

2 1.25E-03 61 0.26 0 0 0 1.00E-02

5 1 15.9 0 0 0 0 0.00E+00 NA

2 1.20E-03 61.1 0.26 0 0 0 1.05E-02

5 2 15.4 2000 0.39 0.09 1.2 1.01E-02 1.52E-03 0.2 4.71E+03 NA

2 1.16E-03 61.1 0.23 0.02 0.33 4.37E-03 4.14E-04 0.31 1.08E-02 15.2

5 3 15.1 0 0 0 0 0.00E+00 NA

2 1.13E-03 61.2 0.23 0 0 0 1.11E-02

5 4 14.5 2197 0.65 0.1 0.51 1.47E-02 5.74E-04 0.38 4.84E+03 NA

2 1.09E-03 61.3 0.25 0.04 0.22 4.07E-03 2.49E-04 0.34 1.16E-02 23.5

5 5 14.2 0 0 0 0 0.00E+00 NA

2 1.06E-03 61.3 0.24 0 0 0 1.18E-02

5 6 14 2395 0.65 0.13 0.36 1.28E-02 3.51E-04 0.32 5.10E+03 NA

2 1.05E-03 61.4 0.28 0.04 0.21 3.95E-03 2.02E-04 0.38 1.20E-02 29.9

5 7 13.8 0 0 0 0 0.00E+00 NA

2 1.03E-03 61.4 0.23 0 0 0 1.22E-02

5 8 13.5 2593 0.81 0.16 0.42 1.40E-02 3.66E-04 0.36 5.33E+03 NA

2 1.01E-03 61.4 0.32 0.06 -0.03 4.03E-03 -2.41E-05 0.41 1.24E-02 -3.8

5 9 13 0 0 0 0 0.00E+00 NA

2 9.78E-04 61.5 0.24 0 0 0 1.28E-02

5 10 12.8 2789 0.92 0.18 0.4 1.45E-02 3.17E-04 0.39 5.45E+03 NA

2 9.64E-04 61.6 0.33 0.07 0.11 3.83E-03 8.30E-05 0.44 1.30E-02 14.7

5 11 12.7 0 0 0 0 0.00E+00 NA 39

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 9.56E-04 61.6 0.25 0 0 0 1.31E-02

5 12 12.6 2986 1.07 0.22 0.33 1.50E-02 2.28E-04 0.4 5.73E+03 NA

2 9.47E-04 61.6 0.39 0.09 0.07 4.01E-03 4.86E-05 0.47 1.33E-02 12

5 13 12.5 0 0 0 0 0.00E+00 NA

2 9.41E-04 61.7 0.23 0 0 0 1.33E-02

5 14 12.4 3178 1.13 0.27 0.47 1.42E-02 2.94E-04 0.36 6.00E+03 NA

2 9.32E-04 61.7 0.45 0.1 0.08 4.09E-03 5.03E-05 0.5 1.35E-02 9.7

5 15 12.4 0 0 0 0 0.00E+00 NA

2 9.28E-04 61.7 0.26 0 0 0 1.35E-02

5 16 12.3 3374 1.25 0.33 0.42 1.41E-02 2.35E-04 0.34 6.31E+03 NA

2 9.23E-04 61.7 0.51 0.11 0.08 4.21E-03 4.39E-05 0.53 1.36E-02 10.6

5 17 12.3 0 0 0 0 0.00E+00 NA

2 9.22E-04 61.8 0.26 0 0 0 1.36E-02

5 18 13.8 0 0 0 0 0.00E+00 NA

2 1.03E-03 62.6 0.26 0 0 0 1.21E-02

5 19 13.9 3378 1.65 0.37 0.33 1.65E-02 1.61E-04 0.44 7.14E+03 NA

2 1.04E-03 62.6 0.58 0.16 -0.57 4.20E-03 -2.85E-04 0.53 1.20E-02 -60.5

5 20 14.6 0 0 0 0 0.00E+00 NA

2 1.10E-03 62.7 0.23 0 0 0 1.14E-02

5 21 15.4 3174 1.35 0.33 0.33 1.38E-02 1.69E-04 0.35 7.46E+03 NA

2 1.15E-03 62.7 0.54 0.11 0.03 4.05E-03 1.49E-05 0.5 1.08E-02 5

5 22 16.1 0 0 0 0 0.00E+00 NA

2 1.21E-03 62.7 0.24 0 0 0 1.03E-02

5 23 16.8 2983 1.3 0.29 0.1 1.37E-02 5.35E-05 0.36 7.68E+03 NA

2 1.26E-03 62.8 0.51 0.1 -0.08 3.92E-03 -4.22E-05 0.47 9.89E-03 -38.3

5 24 19.7 0 0 0 0 0.00E+00 NA

2 1.47E-03 63 0.25 0 0 0 8.45E-03

6 1 19.7 0 0 0 0 0.00E+00 NA

2 1.47E-03 63 0.25 0 0 0 8.45E-03

6 2 20.9 2980 1.65 0.35 0.21 1.41E-02 8.89E-05 0.38 9.52E+03 NA

2 1.56E-03 63.1 0.62 0.13 0.19 3.86E-03 7.87E-05 0.47 7.97E-03 41.5

6 3 25.4 2979 2.18 0.42 0.76 1.52E-02 2.65E-04 0.43 1.16E+04 NA

40

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 1.90E-03 63.3 0.74 0.18 0.72 3.80E-03 2.50E-04 0.47 6.53E-03 43.4

6 4 25.9 2979 2.3 0.43 0.86 1.58E-02 2.93E-04 0.45 1.18E+04 NA

2 1.94E-03 63.3 0.76 0.19 0.8 3.81E-03 2.75E-04 0.47 6.41E-03 43.2

6 5 26.3 2979 2.35 0.43 0.88 1.59E-02 2.96E-04 0.46 1.20E+04 NA

2 1.97E-03 63.3 0.77 0.2 0.68 3.80E-03 2.28E-04 0.47 6.32E-03 37.6

6 6 26.6 2979 2.36 0.44 0.88 1.58E-02 2.91E-04 0.45 1.22E+04 NA

2 1.99E-03 63.3 0.78 0.2 0.61 3.79E-03 2.04E-04 0.47 6.23E-03 35

6 7 27 2980 2.41 0.45 0.93 1.59E-02 3.04E-04 0.46 1.23E+04 NA

2 2.02E-03 63.3 0.79 0.2 0.72 3.79E-03 2.37E-04 0.47 6.14E-03 37.9

6 8 27.4 2979 2.48 0.45 1.04 1.61E-02 3.35E-04 0.47 1.25E+04 NA

2 2.05E-03 63.3 0.8 0.21 0.88 3.81E-03 2.83E-04 0.47 6.05E-03 40.2

6 9 27.8 2979 2.5 0.46 0.96 1.60E-02 3.04E-04 0.46 1.27E+04 NA

2 2.08E-03 63.3 0.82 0.21 0.7 3.81E-03 2.23E-04 0.47 5.96E-03 36.3

6 10 28.2 2979 2.53 0.47 1.02 1.59E-02 3.21E-04 0.45 1.29E+04 NA

2 2.11E-03 63.4 0.83 0.21 0.96 3.85E-03 3.01E-04 0.47 5.87E-03 43.2

6 11 28.6 2979 2.61 0.51 1.1 1.62E-02 3.40E-04 0.44 1.31E+04 NA

2 2.14E-03 63.4 0.9 0.22 0.98 4.09E-03 3.02E-04 0.47 5.79E-03 41.6

6 12 29.1 2980 2.66 0.48 1.17 1.63E-02 3.55E-04 0.47 1.33E+04 NA

2 2.18E-03 63.4 0.85 0.23 0.93 3.79E-03 2.83E-04 0.47 5.70E-03 38.6

6 13 29.5 2980 2.71 0.49 1.06 1.63E-02 3.18E-04 0.48 1.35E+04 NA

2 2.21E-03 63.4 0.86 0.23 0.88 3.79E-03 2.62E-04 0.47 5.61E-03 39.5

6 14 29.9 2980 2.7 0.49 1.19 1.61E-02 3.52E-04 0.47 1.37E+04 NA

2 2.24E-03 63.4 0.87 0.23 1.15 3.77E-03 3.41E-04 0.47 5.54E-03 44

6 15 30.3 2980 2.79 0.5 1.24 1.64E-02 3.61E-04 0.48 1.39E+04 NA

2 2.27E-03 63.4 0.88 0.24 1.02 3.78E-03 2.98E-04 0.47 5.47E-03 39.5

6 16 30.7 2980 2.85 0.53 1.12 1.65E-02 3.24E-04 0.47 1.40E+04 NA

2 2.29E-03 63.5 0.93 0.25 1.11 3.95E-03 3.19E-04 0.47 5.40E-03 44.5

6 17 32.4 2980 3.08 0.54 1.24 1.69E-02 3.39E-04 0.5 1.49E+04 NA

2 2.43E-03 63.5 0.96 0.27 1.18 3.84E-03 3.22E-04 0.47 5.11E-03 43.6

6 18 33 2980 3.04 0.57 1.28 1.64E-02 3.43E-04 0.46 1.51E+04 NA

2 2.47E-03 63.6 1.01 0.26 1.28 3.96E-03 3.44E-04 0.47 5.01E-03 45.1

6 19 33.5 2980 3.16 0.55 1.21 1.68E-02 3.19E-04 0.5 1.53E+04 NA

2 2.50E-03 63.6 0.98 0.28 1.21 3.79E-03 3.21E-04 0.47 4.95E-03 45.1 41

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

6 20 34.4 2980 3.22 0.57 1.33 1.67E-02 3.42E-04 0.49 1.58E+04 NA

2 2.57E-03 63.6 1.01 0.28 1.44 3.80E-03 3.70E-04 0.47 4.81E-03 47.2

6 21 34.8 2980 3.24 0.59 1.32 1.66E-02 3.37E-04 0.48 1.59E+04 NA

2 2.60E-03 63.6 1.03 0.28 1.39 3.86E-03 3.54E-04 0.47 4.76E-03 46.4

6 22 35.1 2980 3.33 0.58 1.39 1.69E-02 3.50E-04 0.5 1.61E+04 NA

2 2.63E-03 63.7 1.03 0.29 1.47 3.80E-03 3.70E-04 0.47 4.71E-03 46.6

6 23 35.5 2980 3.32 0.59 1.38 1.67E-02 3.45E-04 0.49 1.63E+04 NA

2 2.65E-03 63.7 1.04 0.29 1.57 3.80E-03 3.91E-04 0.47 4.66E-03 48.5

6 24 35.8 2980 3.35 0.59 1.41 1.66E-02 3.48E-04 0.49 1.64E+04 NA

2 2.68E-03 63.7 1.04 0.29 1.48 3.78E-03 3.66E-04 0.47 4.62E-03 46.5

6 25 36.2 2980 3.42 0.61 1.37 1.68E-02 3.35E-04 0.49 1.66E+04 NA

2 2.71E-03 63.7 1.07 0.3 1.54 3.84E-03 3.75E-04 0.47 4.57E-03 48.3

6 26 36.6 2980 3.49 0.61 1.36 1.70E-02 3.28E-04 0.51 1.68E+04 NA

2 2.73E-03 63.7 1.07 0.31 1.42 3.80E-03 3.44E-04 0.47 4.53E-03 46.4

6 27 36.9 2980 3.48 0.61 1.41 1.68E-02 3.39E-04 0.5 1.69E+04 NA

2 2.76E-03 63.7 1.08 0.3 1.64 3.81E-03 3.94E-04 0.47 4.48E-03 49.3

6 28 37.2 2980 3.49 0.62 1.45 1.67E-02 3.45E-04 0.49 1.71E+04 NA

2 2.79E-03 63.8 1.09 0.3 1.57 3.83E-03 3.73E-04 0.47 4.44E-03 47.3

6 29 37.6 2980 3.58 0.63 1.42 1.70E-02 3.33E-04 0.5 1.72E+04 NA

2 2.81E-03 63.8 1.1 0.31 1.61 3.82E-03 3.79E-04 0.47 4.40E-03 48.7

6 30 38.1 2980 3.66 0.64 1.35 1.71E-02 3.13E-04 0.5 1.74E+04 NA

2 2.85E-03 63.8 1.14 0.32 1.65 3.89E-03 3.84E-04 0.47 4.35E-03 50.8

6 31 38.4 2980 3.69 0.64 1.48 1.71E-02 3.40E-04 0.51 1.76E+04 NA

2 2.87E-03 63.8 1.12 0.33 1.68 3.81E-03 3.87E-04 0.47 4.31E-03 48.7

6 32 38.8 2980 3.71 0.65 1.59 1.70E-02 3.62E-04 0.5 1.78E+04 NA

2 2.90E-03 63.8 1.14 0.33 1.82 3.84E-03 4.15E-04 0.47 4.27E-03 48.9

6 33 39.1 2980 3.8 0.65 1.46 1.73E-02 3.30E-04 0.52 1.80E+04 NA

2 2.93E-03 63.9 1.15 0.34 1.7 3.82E-03 3.83E-04 0.47 4.23E-03 49.3

6 34 39.5 2980 3.84 0.66 1.43 1.73E-02 3.20E-04 0.52 1.81E+04 NA

2 2.96E-03 63.9 1.16 0.34 1.66 3.81E-03 3.71E-04 0.47 4.19E-03 49.3

6 35 39.9 2980 3.83 0.66 1.43 1.71E-02 3.16E-04 0.51 1.83E+04 NA

2 2.98E-03 63.9 1.17 0.34 1.84 3.81E-03 4.09E-04 0.47 4.15E-03 52.3

6 36 40.2 2980 3.85 0.67 1.39 1.70E-02 3.06E-04 0.51 1.85E+04 NA

42

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 3.01E-03 63.9 1.18 0.34 1.74 3.81E-03 3.82E-04 0.47 4.11E-03 51.3

6 37 40.6 2980 3.94 0.68 1.58 1.73E-02 3.44E-04 0.51 1.86E+04 NA

2 3.03E-03 63.9 1.21 0.35 1.73 3.87E-03 3.78E-04 0.47 4.08E-03 47.7

6 38 40.9 2980 3.93 0.7 1.67 1.71E-02 3.62E-04 0.49 1.88E+04 NA

2 3.06E-03 63.9 1.24 0.35 1.82 3.93E-03 3.94E-04 0.47 4.04E-03 47.4

6 39 41.3 2980 4.05 0.69 1.53 1.74E-02 3.27E-04 0.52 1.89E+04 NA

2 3.09E-03 64 1.21 0.36 1.96 3.82E-03 4.21E-04 0.47 4.01E-03 52.2

6 40 41.7 2981 4.04 0.69 1.56 1.72E-02 3.32E-04 0.52 1.91E+04 NA

2 3.12E-03 64 1.22 0.36 1.83 3.80E-03 3.89E-04 0.47 3.97E-03 49.5

6 41 42 2981 4.06 0.7 1.43 1.72E-02 3.00E-04 0.52 1.93E+04 NA

2 3.14E-03 64 1.23 0.36 1.76 3.80E-03 3.70E-04 0.47 3.94E-03 50.9

6 42 42.4 2981 4.09 0.7 1.58 1.72E-02 3.29E-04 0.51 1.94E+04 NA

2 3.17E-03 64 1.24 0.36 1.86 3.81E-03 3.88E-04 0.47 3.90E-03 49.7

6 43 42.8 2981 4.17 0.71 1.49 1.74E-02 3.07E-04 0.52 1.96E+04 NA

2 3.20E-03 64 1.25 0.37 2.01 3.81E-03 4.15E-04 0.47 3.87E-03 53.5

6 44 43.1 2981 4.17 0.72 1.6 1.72E-02 3.28E-04 0.51 1.98E+04 NA

2 3.22E-03 64.1 1.26 0.37 2.08 3.81E-03 4.26E-04 0.47 3.83E-03 52.3

6 45 44 2981 4.25 0.73 1.38 1.72E-02 2.76E-04 0.51 2.02E+04 NA

2 3.29E-03 64.1 1.29 0.38 2.03 3.81E-03 4.09E-04 0.47 3.76E-03 55.9

6 46 45.8 2980 4.44 0.78 1.43 1.73E-02 2.76E-04 0.5 2.10E+04 NA

2 3.42E-03 64.2 1.37 0.39 2.15 3.90E-03 4.15E-04 0.47 3.61E-03 56.4

6 47 46.2 2980 4.5 0.78 1.5 1.73E-02 2.86E-04 0.51 2.12E+04 NA

2 3.45E-03 64.2 1.37 0.4 2.2 3.85E-03 4.21E-04 0.47 3.58E-03 55.8

6 48 46.6 2980 4.5 0.78 1.55 1.72E-02 2.95E-04 0.51 2.14E+04 NA

2 3.48E-03 64.2 1.37 0.4 2.35 3.83E-03 4.46E-04 0.47 3.55E-03 56.5

6 49 47.2 2980 4.56 0.79 1.49 1.72E-02 2.79E-04 0.51 2.17E+04 NA

2 3.53E-03 64.3 1.39 0.4 2.16 3.84E-03 4.04E-04 0.47 3.50E-03 55.4

6 50 47.7 2981 4.63 0.8 1.33 1.73E-02 2.47E-04 0.51 2.19E+04 NA

2 3.57E-03 64.3 1.4 0.41 2.13 3.83E-03 3.95E-04 0.47 3.47E-03 58

6 51 48.1 2981 4.67 0.81 1.41 1.73E-02 2.59E-04 0.51 2.21E+04 NA

2 3.60E-03 64.3 1.43 0.41 2.29 3.86E-03 4.21E-04 0.47 3.44E-03 58.4

6 52 48.6 2981 4.75 0.82 1.47 1.74E-02 2.68E-04 0.51 2.23E+04 NA

2 3.63E-03 64.4 1.45 0.42 2.37 3.87E-03 4.32E-04 0.47 3.40E-03 58.1 43

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

6 53 49 2981 4.74 0.82 1.38 1.72E-02 2.49E-04 0.51 2.25E+04 NA

2 3.66E-03 64.4 1.44 0.42 2.28 3.83E-03 4.12E-04 0.47 3.37E-03 58.8

6 54 49.5 2981 4.81 0.83 1.48 1.73E-02 2.65E-04 0.52 2.27E+04 NA

2 3.69E-03 64.4 1.46 0.43 2.35 3.84E-03 4.21E-04 0.47 3.35E-03 57.8

6 55 50 2981 4.88 0.84 1.19 1.74E-02 2.10E-04 0.52 2.29E+04 NA

2 3.73E-03 64.4 1.47 0.43 2.22 3.84E-03 3.92E-04 0.47 3.31E-03 61.8

6 56 50.8 2981 4.97 0.86 1.32 1.74E-02 2.29E-04 0.51 2.33E+04 NA

2 3.80E-03 64.5 1.51 0.44 2.45 3.87E-03 4.26E-04 0.47 3.25E-03 61.7

6 57 51.3 2981 4.98 0.86 1.31 1.73E-02 2.26E-04 0.51 2.35E+04 NA

2 3.83E-03 64.5 1.51 0.44 2.43 3.84E-03 4.20E-04 0.47 3.23E-03 61.7

6 58 51.7 2981 5.05 0.86 1.14 1.74E-02 1.95E-04 0.52 2.37E+04 NA

2 3.86E-03 64.5 1.52 0.45 2.3 3.83E-03 3.94E-04 0.47 3.20E-03 63.7

6 59 52.1 2981 5.06 0.87 1.15 1.73E-02 1.95E-04 0.51 2.39E+04 NA

2 3.89E-03 64.5 1.54 0.45 2.55 3.84E-03 4.33E-04 0.47 3.18E-03 65.8

6 60 52.5 2981 5.14 0.88 1.17 1.74E-02 1.97E-04 0.52 2.41E+04 NA

2 3.92E-03 64.5 1.56 0.46 2.42 3.86E-03 4.08E-04 0.47 3.15E-03 64.3

6 61 53.3 2981 5.17 0.89 1.24 1.73E-02 2.06E-04 0.52 2.45E+04 NA

2 3.98E-03 64.6 1.57 0.46 2.51 3.82E-03 4.17E-04 0.47 3.10E-03 63.6

6 62 54.1 2981 5.26 0.93 1.16 1.73E-02 1.89E-04 0.5 2.48E+04 NA

2 4.04E-03 64.6 1.63 0.47 2.65 3.93E-03 4.33E-04 0.47 3.06E-03 66.4

6 63 54.5 2981 5.24 0.92 1.28 1.71E-02 2.09E-04 0.5 2.50E+04 NA

2 4.07E-03 64.6 1.62 0.46 2.97 3.88E-03 4.83E-04 0.47 3.04E-03 66.6

6 64 55 2981 5.42 0.94 0.93 1.75E-02 1.49E-04 0.52 2.52E+04 NA

2 4.11E-03 64.7 1.65 0.48 2.63 3.90E-03 4.24E-04 0.47 3.01E-03 70.6

6 65 55.5 2981 5.42 0.94 1.27 1.74E-02 2.03E-04 0.51 2.55E+04 NA

2 4.15E-03 64.7 1.66 0.48 2.79 3.89E-03 4.44E-04 0.47 2.98E-03 65.4

6 66 55.9 2981 5.38 0.94 1.16 1.72E-02 1.83E-04 0.51 2.56E+04 NA

2 4.17E-03 64.7 1.65 0.47 2.88 3.84E-03 4.57E-04 0.47 2.96E-03 68.2

6 67 56.3 2981 5.46 0.95 1.09 1.73E-02 1.71E-04 0.51 2.58E+04 NA

2 4.20E-03 64.7 1.67 0.48 2.82 3.86E-03 4.43E-04 0.47 2.94E-03 68.9

6 68 56.9 2981 5.54 0.96 1.04 1.74E-02 1.62E-04 0.51 2.61E+04 NA

2 4.25E-03 64.7 1.69 0.49 2.76 3.87E-03 4.29E-04 0.47 2.91E-03 69.4

6 69 57.4 2981 5.55 0.97 0.84 1.72E-02 1.31E-04 0.51 2.63E+04 NA

44

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 4.28E-03 64.8 1.71 0.49 3.13 3.88E-03 4.84E-04 0.47 2.89E-03 74.9

6 70 57.7 2981 5.6 0.97 0.86 1.73E-02 1.32E-04 0.51 2.65E+04 NA

2 4.31E-03 64.8 1.72 0.5 3 3.87E-03 4.61E-04 0.47 2.87E-03 74.1

6 71 58.1 2981 5.62 0.98 0.8 1.72E-02 1.22E-04 0.51 2.67E+04 NA

2 4.34E-03 64.8 1.72 0.5 2.91 3.86E-03 4.43E-04 0.47 2.85E-03 74.7

6 72 58.8 2981 5.75 1 0.81 1.74E-02 1.22E-04 0.51 2.69E+04 NA

2 4.39E-03 64.8 1.77 0.51 2.69 3.92E-03 4.05E-04 0.47 2.82E-03 73.3

6 73 59.1 2981 5.79 1 0.97 1.75E-02 1.45E-04 0.52 2.71E+04 NA

2 4.41E-03 64.8 1.75 0.51 3.01 3.87E-03 4.51E-04 0.47 2.80E-03 72.1

6 74 59.5 2981 5.79 1 0.82 1.73E-02 1.22E-04 0.51 2.73E+04 NA

2 4.44E-03 64.8 1.76 0.51 2.88 3.85E-03 4.29E-04 0.47 2.78E-03 74.2

6 75 59.9 2981 5.82 1 0.72 1.73E-02 1.06E-04 0.51 2.75E+04 NA

2 4.47E-03 64.9 1.77 0.52 2.7 3.85E-03 3.99E-04 0.47 2.76E-03 75.1

6 76 60.3 2981 5.89 1.02 0.59 1.74E-02 8.62E-05 0.51 2.77E+04 NA

2 4.50E-03 64.9 1.79 0.52 2.8 3.87E-03 4.11E-04 0.47 2.74E-03 78.2

6 77 60.7 2981 5.92 1.03 0.47 1.74E-02 6.86E-05 0.51 2.78E+04 NA

2 4.53E-03 64.9 1.82 0.53 2.98 3.91E-03 4.35E-04 0.47 2.73E-03 81

6 78 61 2981 5.99 1.04 0.58 1.75E-02 8.40E-05 0.51 2.80E+04 NA

2 4.55E-03 64.9 1.83 0.53 2.75 3.91E-03 4.00E-04 0.47 2.71E-03 78.1

6 79 61.4 2981 6.01 1.04 0.57 1.74E-02 8.25E-05 0.52 2.82E+04 NA

2 4.58E-03 64.9 1.83 0.53 2.98 3.87E-03 4.30E-04 0.47 2.69E-03 79.1

6 80 61.8 2981 6.04 1.05 0.4 1.74E-02 5.77E-05 0.51 2.83E+04 NA

2 4.61E-03 64.9 1.85 0.54 2.85 3.91E-03 4.09E-04 0.47 2.68E-03 82

6 81 62.2 2981 6.06 1.05 0.45 1.74E-02 6.47E-05 0.51 2.85E+04 NA

2 4.64E-03 64.9 1.85 0.54 3.04 3.87E-03 4.33E-04 0.47 2.66E-03 81.5

6 82 62.5 2981 6.15 1.06 0.71 1.75E-02 1.00E-04 0.52 2.87E+04 NA

2 4.67E-03 65 1.86 0.55 2.87 3.89E-03 4.07E-04 0.47 2.65E-03 76.2

6 83 62.9 2981 6.16 1.06 0.45 1.75E-02 6.31E-05 0.52 2.88E+04 NA

2 4.69E-03 65 1.87 0.55 2.86 3.87E-03 4.04E-04 0.47 2.63E-03 81.1

6 84 63.2 2981 6.13 1.06 0.49 1.73E-02 6.80E-05 0.51 2.90E+04 NA

2 4.72E-03 65 1.87 0.54 3.09 3.85E-03 4.33E-04 0.47 2.62E-03 81.1

6 85 63.6 2981 6.23 1.08 0.26 1.75E-02 3.66E-05 0.51 2.92E+04 NA

2 4.75E-03 65 1.9 0.55 2.99 3.89E-03 4.17E-04 0.47 2.60E-03 85 45

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

6 86 64 2981 6.23 1.08 0.41 1.74E-02 5.70E-05 0.51 2.93E+04 NA

2 4.77E-03 65 1.9 0.55 3.04 3.87E-03 4.21E-04 0.47 2.59E-03 82.3

6 87 64.4 2981 6.25 1.09 0.22 1.73E-02 3.00E-05 0.51 2.95E+04 NA

2 4.80E-03 65 1.91 0.55 3.18 3.87E-03 4.38E-04 0.47 2.57E-03 86.1

6 88 65.5 0 0 0 0 0.00E+00 NA

2 4.88E-03 65.1 0.25 0 0 0 2.53E-03

7 1 1015.6 0 0 0 0 0.00E+00 NA

2 7.44E-02 74.5 0.35 0 0 0 1.65E-04

7 2 1015.6 500 3.19 0.1 -1.26 2.03E-02 -3.98E-04 0.49 7.70E+04 4.8

2 7.44E-02 74.5 1.09 0.05 1.23 5.09E-03 3.87E-04 0.08 1.65E-04 135.8

7 3 1015.6 1000 13.5 0.66 -4.49 2.14E-02 -3.55E-04 0.68 1.54E+05 9.3

2 7.44E-02 74.5 3.47 0.45 5.41 4.03E-03 4.27E-04 0.15 1.65E-04 129.7

7 4 1015.6 1248 21.13 1.23 -5.7 2.15E-02 -2.89E-04 0.71 1.92E+05 11.5

2 7.44E-02 74.5 5.19 0.87 11.82 3.87E-03 5.99E-04 0.19 1.65E-04 115.7

7 5 1015.6 0 0 0 0 0.00E+00 NA

2 7.44E-02 74.5 0.44 0 0 0 1.65E-04

8 1 1019.5 0 0 0 0 0.00E+00 0

1 7.55E-02 69.3 0.28 0 0 0 1.62E-04

8 2 1019.5 1003 8.09 0.3 -3.14 1.26E-02 -2.43E-04 0.68 1.57E+05 7.2

1 7.55E-02 69.3 1.59 0.21 2.23 1.81E-03 1.73E-04 0.16 1.62E-04 144.6

8 3 1019.5 1495 18.65 0.98 -9.26 1.31E-02 -3.23E-04 0.73 2.34E+05 11.2

1 7.55E-02 69.3 3.44 0.72 6.75 1.76E-03 2.35E-04 0.23 1.62E-04 143.9

8 4 1019.5 2084 36.34 2.66 -14.03 1.31E-02 -2.52E-04 0.74 3.26E+05 15.2

1 7.55E-02 69.3 6.7 1.96 14.14 1.77E-03 2.54E-04 0.32 1.62E-04 134.8

8 5 1019.5 0 0 0 0 0.00E+00 NA

1 7.55E-02 69.3 0.32 0 0 0 1.62E-04

9 1 743.3 0 0.03 0 -0.56 0.00E+00 4.8

1 5.57E-02 62.4 -0.01 0 -0.2 0 2.18E-04 -160.1

9 2 601.6 0 -0.09 0 -0.56 0.00E+00 4.9

1 4.55E-02 58.3 -0.01 0 -1.27 0 2.65E-04 66.4

46

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

9 3 575.5 0 -0.09 0 -0.69 0.00E+00 3.1

1 4.37E-02 56 -0.01 0 -1.26 0 2.75E-04 61.4

9 4 562.4 0 -0.1 0 -0.69 0.00E+00 2

1 4.28E-02 54.7 -0.01 0 -1.22 0 2.80E-04 60.4

9 5 110.1 0 0 0 0 0.00E+00 NA

1 8.23E-03 64.4 0.27 0 0 0 1.50E-03

9 6 112.1 1986 3.11 0.37 -0.35 1.11E-02 -6.19E-05 0.4 3.44E+04 7.5

1 8.37E-03 64.5 0.99 0.15 0.57 2.58E-03 1.02E-04 0.31 1.47E-03 121.2

9 7 112.9 2185 3.86 0.4 -0.54 1.13E-02 -7.82E-05 0.5 3.81E+04 10

1 8.43E-03 64.5 0.97 0.2 0.66 2.08E-03 9.66E-05 0.34 1.46E-03 129

9 8 113.8 2383 4.69 0.52 -0.97 1.15E-02 -1.18E-04 0.52 4.19E+04 12.3

1 8.50E-03 64.6 1.14 0.27 0.93 2.05E-03 1.13E-04 0.37 1.45E-03 136.3

9 9 114.9 2580 5.65 0.77 -1.69 1.17E-02 -1.74E-04 0.46 4.58E+04 14.4

1 8.58E-03 64.6 1.56 0.36 0.93 2.37E-03 9.54E-05 0.4 1.44E-03 151.2

9 10 115.7 2778 6.72 0.94 -1.96 1.19E-02 -1.73E-04 0.49 4.96E+04 16.5

1 8.64E-03 64.6 1.78 0.46 1.03 2.30E-03 9.03E-05 0.43 1.43E-03 152.4

9 11 116.6 2976 7.86 1.12 -2.04 1.21E-02 -1.56E-04 0.52 5.35E+04 17.9

1 8.70E-03 64.7 1.98 0.58 1.44 2.22E-03 1.09E-04 0.47 1.42E-03 144.9

9 12 117.6 3177 9.21 1.25 -3.41 1.23E-02 -2.26E-04 0.59 5.76E+04 20

1 8.78E-03 64.7 2.07 0.73 2.09 2.02E-03 1.39E-04 0.5 1.40E-03 148.5

9 13 118.6 3367 10.47 1.52 -4.33 1.23E-02 -2.54E-04 0.58 6.16E+04 21.6

1 8.85E-03 64.8 2.37 0.88 2.54 2.04E-03 1.49E-04 0.53 1.39E-03 149.6

9 14 119.9 0 0 0 0 0.00E+00 NA

1 8.94E-03 64.9 0.27 0 0 0 1.38E-03

10 1 120.6 0 0 0 0 0.00E+00 NA

1 9.00E-03 64.9 0.02 0 0 0 1.37E-03

10 2 127 2541 7.22 0.78 -2.86 1.40E-02 -2.75E-04 0.63 4.97E+04 16.7

1 9.47E-03 65.3 1.6 0.49 2.34 2.27E-03 2.24E-04 0.4 1.30E-03 140.7

10 3 132.4 2975 8.95 1.13 -2.95 1.21E-02 -1.98E-04 0.59 6.06E+04 19.1

1 9.87E-03 65.6 1.99 0.66 2.58 1.97E-03 1.73E-04 0.46 1.25E-03 138.8

10 4 137.9 2975 9.38 1.19 -2.64 1.22E-02 -1.71E-04 0.59 6.31E+04 19.3

1 1.03E-02 66 2.1 0.7 2.69 2.00E-03 1.74E-04 0.46 1.20E-03 134.4 47

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

10 5 143.2 2974 9.77 1.24 -2.59 1.22E-02 -1.61E-04 0.59 6.55E+04 19.5

1 1.07E-02 66.3 2.19 0.73 2.8 2.00E-03 1.74E-04 0.46 1.16E-03 132.7

10 6 148.7 2974 10.17 1.27 -2.76 1.23E-02 -1.66E-04 0.59 6.79E+04 19.7

1 1.11E-02 66.6 2.25 0.76 2.99 1.98E-03 1.80E-04 0.46 1.11E-03 132.6

10 7 154.6 2974 10.59 1.32 -3.1 1.23E-02 -1.79E-04 0.6 7.06E+04 19.9

1 1.15E-02 66.9 2.34 0.79 3.2 1.99E-03 1.85E-04 0.46 1.07E-03 134.1

10 8 164.3 2974 11.11 1.39 -3.26 1.22E-02 -1.77E-04 0.59 7.49E+04 20.1

1 1.22E-02 67.3 2.46 0.82 3.71 1.97E-03 2.02E-04 0.46 1.01E-03 131.3

10 9 169.6 2974 11.47 1.45 -3.64 1.22E-02 -1.92E-04 0.59 7.73E+04 20.2

1 1.26E-02 67.6 2.56 0.85 3.6 1.99E-03 1.90E-04 0.46 9.80E-04 135.3

10 10 174.8 2974 11.73 1.48 -4.1 1.21E-02 -2.10E-04 0.58 7.96E+04 20.3

1 1.30E-02 67.8 2.62 0.87 3.57 1.97E-03 1.83E-04 0.46 9.51E-04 138.9

10 11 180.1 0 0 0 0 0.00E+00 NA

1 1.34E-02 68.1 0.27 0 0 0 9.23E-04

11 1 1012.6 0 0 0 0 0.00E+00 NA

1 7.43E-02 74 0.36 0 0 0 1.66E-04

11 2 1012.7 1000 8 0.34 -3.42 1.27E-02 -2.71E-04 0.61 1.53E+05 7.1

1 7.43E-02 73.8 1.77 0.2 2.98 2.05E-03 2.36E-04 0.16 1.66E-04 138.9

11 3 1012.6 1494 18.56 1.05 -7.76 1.32E-02 -2.75E-04 0.69 2.29E+05 10.8

1 7.43E-02 73.6 3.69 0.72 6.32 1.92E-03 2.24E-04 0.23 1.66E-04 140.8

11 4 1012.6 2092 36.74 2.75 -15.38 1.33E-02 -2.78E-04 0.73 3.21E+05 15.8

1 7.43E-02 73.5 6.91 2 14.07 1.83E-03 2.54E-04 0.32 1.66E-04 137.6

11 5 1012.6 0 0 0 0 0.00E+00 NA

1 7.44E-02 73.3 0.42 0 0 0 1.66E-04

12 1 1016.3 0 0 0 0 0.00E+00 NA

1 7.52E-02 69.3 0.29 0 0 0 1.63E-04

12 2 1016.3 500 2.04 0.04 -0.88 1.28E-02 -2.76E-04 0.68 7.80E+04 3.6

1 7.52E-02 69.3 0.4 0.03 0.9 1.86E-03 2.81E-04 0.08 1.63E-04 134.4

12 3 1016.2 1201 11.81 0.5 -5.06 1.29E-02 -2.74E-04 0.72 1.87E+05 8.7

1 7.52E-02 69.3 2.2 0.36 4.68 1.75E-03 2.54E-04 0.19 1.63E-04 137.2

12 4 1016.2 1594 21.28 1.17 -9.23 1.32E-02 -2.84E-04 0.75 2.49E+05 11.8

48

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 7.52E-02 69.3 3.87 0.88 8.09 1.75E-03 2.49E-04 0.25 1.63E-04 138.8

12 5 1016.2 2091 37.27 2.7 -16.13 1.34E-02 -2.88E-04 0.75 3.26E+05 15.6

1 7.52E-02 69.3 6.79 2.04 14.23 1.78E-03 2.54E-04 0.33 1.63E-04 138.6

12 6 1016.2 0 0.08 0 -0.04 0.00E+00 NA

1 7.52E-02 69.4 0.02 0 -0.08 0 1.63E-04 -114.2

13 1 923.4 0 0.05 0 0.81 0.00E+00 4

1 6.84E-02 68.9 -0.01 0 0.48 0 1.79E-04 30.6

13 2 892.8 0 0.05 0 0.79 0.00E+00 3.9

1 6.62E-02 68.3 -0.01 0 0.5 0 1.85E-04 32.6

13 3 868 0 0.06 0 0.73 0.00E+00 3.8

1 6.44E-02 67.7 -0.01 0 0.53 0 1.90E-04 35.8

13 4 845.1 0 0.06 0 0.7 0.00E+00 3.7

1 6.28E-02 67 -0.01 0 0.53 0 1.95E-04 37.3

13 5 823.6 0 0.06 0 0.65 0.00E+00 3.5

1 6.13E-02 66.2 -0.01 0 0.54 0 1.99E-04 39.6

13 6 804.7 0 0.06 0 0.63 0.00E+00 3.4

1 6.00E-02 65.4 -0.01 0 0.56 0 2.03E-04 41.7

13 7 787.2 0 0.06 0 0.59 0.00E+00 3.3

1 5.87E-02 64.9 -0.01 0 0.57 0 2.07E-04 43.6

13 8 770.2 0 0.06 0 0.56 0.00E+00 3.2

1 5.76E-02 64.1 -0.01 0 0.57 0 2.11E-04 45.5

13 9 754.2 0 0.06 0 0.54 0.00E+00 3

1 5.64E-02 63.4 -0.01 0 0.57 0 2.15E-04 46.9

13 10 738.7 0 0.06 0 0.5 0.00E+00 2.7

1 5.54E-02 62.6 -0.01 0 0.58 0 2.19E-04 49.1

13 11 723.6 0 0.06 0 0.47 0.00E+00 2.4

1 5.43E-02 61.9 -0.01 0 0.59 0 2.23E-04 51.6

13 12 709.4 0 0.06 0 0.45 0.00E+00 2

1 5.33E-02 61.2 -0.01 0 0.6 0 2.27E-04 53.3

13 13 695.6 0 0.06 0 0.41 0.00E+00 1.4

1 5.23E-02 60.6 -0.01 0 0.6 0 2.31E-04 55.6

13 14 682.4 0 0.06 0 0.39 0.00E+00 0.7 49

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 5.14E-02 60.1 -0.01 0 0.61 0 2.36E-04 57.6

13 15 24.6 0 0.04 0 0.08 0.00E+00 28.3

1 1.89E-03 48.2 -0.01 0 -0.12 0 6.40E-03 -56.9

13 16 21 0 0.04 0 0.09 0.00E+00 35.4

1 1.62E-03 48.4 -0.01 0 -0.11 0 7.50E-03 -51.6

13 17 17.8 0 0.05 0 0.09 0.00E+00 40.9

1 1.37E-03 48.5 -0.01 0 -0.1 0 8.89E-03 -47.3

13 18 14.8 0 0 0 0 0.00E+00 NA

1 1.13E-03 54.4 0.26 0 0 0 1.11E-02

13 19 16.3 1989 0.27 0.07 -0.15 6.41E-03 -1.78E-04 0.13 5.03E+03 NA

1 1.24E-03 54.9 0.19 0.01 -0.47 3.36E-03 -5.67E-04 0.31 1.01E-02 -107.5

13 20 17.5 2192 0.38 0.08 -0.2 6.93E-03 -1.84E-04 0.19 5.95E+03 NA

1 1.33E-03 55.2 0.19 0.02 -0.6 2.63E-03 -5.51E-04 0.35 9.37E-03 -108.5

13 21 18.3 2393 0.45 0.1 -0.08 6.63E-03 -5.74E-05 0.2 6.77E+03 NA

1 1.39E-03 55.4 0.21 0.02 -0.68 2.29E-03 -5.05E-04 0.38 9.00E-03 -96.5

13 22 19.6 2587 0.61 0.14 -0.37 7.24E-03 -2.19E-04 0.22 7.85E+03 NA

1 1.49E-03 55.8 0.28 0.03 -0.76 2.45E-03 -4.46E-04 0.41 8.39E-03 -116.1

13 23 20.7 2781 0.77 0.16 -0.51 7.47E-03 -2.46E-04 0.26 8.91E+03 NA

1 1.57E-03 56.1 0.31 0.04 -0.85 2.18E-03 -4.09E-04 0.44 7.94E-03 -121

13 24 21.6 2977 0.99 0.36 -0.34 8.06E-03 -1.38E-04 0.16 9.96E+03 NA

1 1.64E-03 56.3 0.64 0.06 -1.02 3.80E-03 -4.12E-04 0.47 7.61E-03 -108.5

13 25 22.4 3174 1.34 0.4 -0.26 9.21E-03 -8.89E-05 0.23 1.10E+04 NA

1 1.70E-03 56.5 0.67 0.09 -1.6 3.36E-03 -5.49E-04 0.5 7.33E-03 -99.2

13 26 23.1 3378 1.65 0.47 -0.19 9.77E-03 -5.52E-05 0.26 1.21E+04 NA

1 1.75E-03 56.7 0.73 0.12 -1.7 3.17E-03 -5.01E-04 0.53 7.12E-03 -96.3

13 27 24.6 3378 1.9 0.47 0.02 1.06E-02 6.79E-06 0.32 1.29E+04 NA

1 1.86E-03 57.1 0.73 0.15 -1.59 2.95E-03 -4.39E-04 0.53 6.69E-03 -89.1

13 28 25.2 3378 1.99 0.46 0 1.08E-02 9.63E-07 0.34 1.32E+04 NA

1 1.91E-03 57.3 0.72 0.16 -1.48 2.84E-03 -3.99E-04 0.53 6.52E-03 -89.9

13 29 25.8 3378 2.03 0.38 -0.02 1.07E-02 -5.65E-06 0.43 1.35E+04 NA

1 1.96E-03 57.5 0.58 0.16 -1.35 2.26E-03 -3.56E-04 0.53 6.37E-03 -90.9

13 30 26.4 3378 1.99 0.37 -0.42 1.03E-02 -1.09E-04 0.42 1.38E+04 NA

1 2.00E-03 57.6 0.57 0.15 -1.3 2.17E-03 -3.33E-04 0.53 6.23E-03 -108.1

50

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

13 31 27.2 3378 1.98 0.38 -0.79 9.98E-03 -1.98E-04 0.4 1.42E+04 NA

1 2.06E-03 57.8 0.59 0.15 -1.25 2.18E-03 -3.13E-04 0.53 6.05E-03 -122.4

13 32 28 3378 1.99 0.39 -0.91 9.74E-03 -2.20E-04 0.39 1.46E+04 NA

1 2.12E-03 58 0.6 0.15 -1.15 2.15E-03 -2.80E-04 0.53 5.88E-03 -128.2

13 33 28.7 3379 2.01 0.39 -0.92 9.60E-03 -2.19E-04 0.38 1.50E+04 NA

1 2.17E-03 58.2 0.61 0.15 -1.15 2.13E-03 -2.72E-04 0.53 5.74E-03 -128.8

13 34 29.5 3379 2.06 0.4 -0.93 9.57E-03 -2.15E-04 0.38 1.54E+04 NA

1 2.23E-03 58.4 0.63 0.15 -1.08 2.13E-03 -2.49E-04 0.53 5.58E-03 -130.9

13 35 30.2 3378 2.11 0.41 -0.91 9.59E-03 -2.06E-04 0.38 1.58E+04 NA

1 2.28E-03 58.6 0.64 0.16 -1.03 2.12E-03 -2.33E-04 0.53 5.45E-03 -131.5

13 36 31 3379 2.17 0.43 -0.7 9.60E-03 -1.55E-04 0.38 1.62E+04 NA

1 2.34E-03 58.7 0.67 0.16 -0.93 2.17E-03 -2.04E-04 0.53 5.32E-03 -127.3

13 37 31.7 3379 2.23 0.43 -0.55 9.65E-03 -1.19E-04 0.38 1.65E+04 NA

1 2.39E-03 58.9 0.68 0.17 -0.86 2.14E-03 -1.84E-04 0.53 5.21E-03 -123

13 38 33.5 3177 2.12 0.38 0.07 9.80E-03 1.64E-05 0.4 1.64E+04 NA

1 2.53E-03 59.3 0.62 0.15 -0.7 2.10E-03 -1.61E-04 0.5 4.92E-03 -84.2

13 39 34.3 2981 1.87 0.31 0.26 9.61E-03 6.63E-05 0.39 1.58E+04 NA

1 2.58E-03 59.4 0.55 0.12 -0.53 2.07E-03 -1.35E-04 0.47 4.81E-03 -63.8

13 40 35.1 2785 1.7 0.26 0.32 9.79E-03 9.26E-05 0.41 1.51E+04 NA

1 2.64E-03 59.6 0.48 0.11 -0.41 2.04E-03 -1.18E-04 0.44 4.70E-03 -51.9

13 41 35.8 2582 1.51 0.21 0.41 9.96E-03 1.34E-04 0.42 1.43E+04 NA

1 2.70E-03 59.7 0.42 0.09 -0.46 2.03E-03 -1.50E-04 0.41 4.61E-03 -48.2

13 42 36.5 2381 1.32 0.17 0.34 9.99E-03 1.30E-04 0.42 1.34E+04 NA

1 2.75E-03 59.8 0.37 0.07 -0.57 2.04E-03 -2.15E-04 0.37 4.52E-03 -58.8

13 43 37.2 2185 1.14 0.14 0.19 1.01E-02 8.27E-05 0.41 1.26E+04 NA

1 2.80E-03 59.9 0.33 0.06 -0.55 2.15E-03 -2.40E-04 0.34 4.43E-03 -71

13 44 37.9 1992 1.01 0.11 -0.11 1.06E-02 -5.88E-05 0.42 1.17E+04 NA

1 2.86E-03 60 0.29 0.05 -0.41 2.23E-03 -2.14E-04 0.31 4.35E-03 -105.4

13 45 38.6 0 0 0 0 0.00E+00 NA

1 2.91E-03 60.2 0.24 0 0 0 4.27E-03

14 1 38.6 0 0 0 0 0.00E+00 NA

1 2.91E-03 60.2 0.24 0 0 0 4.27E-03 51

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

14 2 39.6 1992 0.88 0.12 -0.23 8.75E-03 -1.13E-04 0.31 1.22E+04 NA

1 2.98E-03 60.3 0.31 0.04 0.19 2.29E-03 9.40E-05 0.31 4.16E-03 140.3

14 3 40.4 2185 1.06 0.15 -0.19 8.67E-03 -7.71E-05 0.33 1.36E+04 NA

1 3.04E-03 60.4 0.36 0.05 0.21 2.14E-03 8.59E-05 0.34 4.08E-03 131.9

14 4 41.1 2381 1.31 0.19 -0.12 8.83E-03 -4.07E-05 0.35 1.51E+04 NA

1 3.09E-03 60.6 0.42 0.07 0.3 2.06E-03 9.99E-05 0.37 4.02E-03 112.2

14 5 42.3 2591 1.61 0.24 0 8.92E-03 -1.22E-06 0.37 1.69E+04 NA

1 3.18E-03 60.7 0.49 0.09 0.47 1.99E-03 1.30E-04 0.41 3.90E-03 90.5

14 6 43 2779 1.87 0.31 0.11 8.88E-03 2.63E-05 0.36 1.84E+04 NA

1 3.23E-03 60.8 0.58 0.11 0.77 2.01E-03 1.82E-04 0.44 3.84E-03 81.8

14 7 43.6 2977 2.21 0.39 0.18 8.99E-03 3.55E-05 0.36 2.00E+04 NA

1 3.28E-03 60.9 0.69 0.14 0.79 2.06E-03 1.60E-04 0.47 3.79E-03 77.5

14 8 44.2 3179 2.6 0.49 0.19 9.16E-03 3.40E-05 0.37 2.17E+04 NA

1 3.33E-03 61 0.81 0.18 0.8 2.07E-03 1.39E-04 0.5 3.73E-03 76.3

14 9 44.8 3378 3.01 0.61 0.18 9.27E-03 2.79E-05 0.36 2.33E+04 NA

1 3.37E-03 61.1 0.94 0.22 0.89 2.13E-03 1.36E-04 0.53 3.69E-03 78.4

14 10 45.4 3181 2.74 0.5 0.27 9.36E-03 4.57E-05 0.38 2.23E+04 NA

1 3.42E-03 61.1 0.83 0.19 0.81 2.08E-03 1.38E-04 0.5 3.63E-03 71.7

14 11 46 2979 2.38 0.41 0.46 9.18E-03 8.85E-05 0.37 2.11E+04 NA

1 3.46E-03 61.2 0.72 0.15 0.69 2.04E-03 1.31E-04 0.47 3.59E-03 56

14 12 46.9 2788 2.14 0.34 0.44 9.26E-03 9.36E-05 0.38 2.01E+04 NA

1 3.52E-03 61.3 0.64 0.13 0.79 2.01E-03 1.71E-04 0.44 3.52E-03 61.3

14 13 47.5 2580 1.86 0.27 0.42 9.28E-03 1.04E-04 0.39 1.89E+04 NA

1 3.57E-03 61.3 0.55 0.1 0.52 2.01E-03 1.29E-04 0.4 3.47E-03 51.1

14 14 48.2 2393 1.63 0.22 0.3 9.28E-03 8.56E-05 0.38 1.78E+04 NA

1 3.62E-03 61.4 0.49 0.08 0.39 2.03E-03 1.10E-04 0.38 3.43E-03 52

14 15 48.8 2187 1.36 0.18 0.22 9.19E-03 7.51E-05 0.36 1.64E+04 NA

1 3.66E-03 61.5 0.43 0.06 0.27 2.10E-03 9.06E-05 0.34 3.38E-03 50.4

14 16 49.4 1994 1.13 0.14 0.19 9.06E-03 7.59E-05 0.35 1.52E+04 NA

1 3.71E-03 61.5 0.37 0.05 0.3 2.15E-03 1.19E-04 0.31 3.35E-03 57.5

14 17 50 0 0 0 0 0.00E+00 NA

1 3.75E-03 61.6 0.24 0 0 0 3.31E-03

52

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

15 1 50 0 0 0 0 0.00E+00 NA

1 3.75E-03 61.6 0.24 0 0 0 3.31E-03

15 2 50.7 1993 1.09 0.15 -0.07 8.54E-03 -2.70E-05 0.31 1.56E+04 NA

1 3.81E-03 61.7 0.38 0.05 0.38 2.19E-03 1.46E-04 0.31 3.25E-03 100.5

15 3 51.4 2185 1.38 0.19 -0.11 8.85E-03 -3.63E-05 0.35 1.73E+04 NA

1 3.86E-03 61.8 0.45 0.06 0.42 2.09E-03 1.35E-04 0.34 3.21E-03 105

15 4 52 2389 1.68 0.24 -0.09 8.93E-03 -2.41E-05 0.36 1.91E+04 NA

1 3.90E-03 61.9 0.52 0.09 0.57 2.03E-03 1.49E-04 0.37 3.18E-03 99.2

15 5 52.6 2587 2.03 0.3 -0.1 9.09E-03 -2.12E-05 0.38 2.10E+04 NA

1 3.95E-03 62 0.61 0.11 0.71 1.98E-03 1.58E-04 0.41 3.14E-03 97.6

15 6 53.8 2787 2.43 0.38 0.01 9.17E-03 1.90E-06 0.38 2.31E+04 NA

1 4.03E-03 62.1 0.72 0.15 1.01 1.99E-03 1.89E-04 0.44 3.07E-03 89.4

15 7 54.5 2975 2.83 0.48 0.07 9.24E-03 1.20E-05 0.38 2.50E+04 5.2

1 4.08E-03 62.1 0.84 0.18 1.02 2.01E-03 1.66E-04 0.47 3.03E-03 85.9

15 8 55.1 3174 3.35 0.6 0.04 9.52E-03 6.14E-06 0.39 2.69E+04 7.7

1 4.13E-03 62.2 1 0.23 1.11 2.08E-03 1.56E-04 0.5 3.00E-03 87.8

15 9 55.6 3373 3.83 0.74 0.13 9.54E-03 1.57E-05 0.39 2.89E+04 11.6

1 4.17E-03 62.2 1.15 0.28 1.3 2.09E-03 1.61E-04 0.53 2.97E-03 84.5

15 10 56.3 3172 3.48 0.65 0.23 9.69E-03 3.17E-05 0.38 2.75E+04 9.6

1 4.22E-03 62.3 1.08 0.25 1.11 2.20E-03 1.54E-04 0.5 2.94E-03 78.4

15 11 56.8 2981 3.04 0.5 0.42 9.51E-03 6.56E-05 0.4 2.61E+04 7.5

1 4.26E-03 62.4 0.89 0.2 1 2.03E-03 1.55E-04 0.47 2.91E-03 67.1

15 12 57.5 2785 2.7 0.41 0.33 9.54E-03 5.77E-05 0.4 2.46E+04 5.5

1 4.31E-03 62.4 0.78 0.17 0.98 2.00E-03 1.72E-04 0.44 2.88E-03 71.5

15 13 58.1 2584 2.32 0.33 0.36 9.45E-03 7.18E-05 0.4 2.31E+04 NA

1 4.36E-03 62.5 0.67 0.13 0.76 1.98E-03 1.54E-04 0.4 2.85E-03 65

15 14 58.8 2386 1.99 0.26 0.23 9.36E-03 5.50E-05 0.39 2.16E+04 NA

1 4.41E-03 62.5 0.58 0.1 0.48 2.00E-03 1.12E-04 0.37 2.81E-03 63.9

15 15 59.4 2188 1.69 0.21 0.16 9.38E-03 4.45E-05 0.38 2.00E+04 NA

1 4.45E-03 62.6 0.51 0.08 0.49 2.05E-03 1.35E-04 0.34 2.79E-03 71.8

15 16 60 1988 1.37 0.16 0.19 9.10E-03 6.13E-05 0.36 1.84E+04 NA

1 4.50E-03 62.6 0.43 0.06 0.51 2.10E-03 1.68E-04 0.31 2.75E-03 70

15 17 60.8 0 0 0 0 0.00E+00 NA 53

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 4.55E-03 62.7 0.26 0 0 0 2.72E-03

16 1 60.8 0 0 0 0 0.00E+00 NA

1 4.55E-03 62.7 0.26 0 0 0 2.72E-03

16 2 61.5 1983 1.37 0.17 -0.27 8.94E-03 -8.62E-05 0.34 1.88E+04 NA

1 4.61E-03 62.8 0.45 0.06 0.62 2.13E-03 2.00E-04 0.31 2.69E-03 113.4

16 3 62.1 2183 1.72 0.22 -0.32 9.17E-03 -8.50E-05 0.37 2.09E+04 NA

1 4.66E-03 62.9 0.53 0.08 0.55 2.06E-03 1.46E-04 0.34 2.66E-03 120.3

16 4 62.7 2384 2.06 0.28 -0.26 9.13E-03 -5.83E-05 0.38 2.30E+04 NA

1 4.69E-03 62.9 0.62 0.11 0.7 2.00E-03 1.55E-04 0.37 2.64E-03 110.6

16 5 63.3 2583 2.51 0.35 -0.4 9.37E-03 -7.43E-05 0.4 2.52E+04 6.7

1 4.74E-03 63 0.72 0.14 0.84 1.97E-03 1.57E-04 0.4 2.61E-03 115.3

16 6 64 2788 2.98 0.46 -0.44 9.46E-03 -6.98E-05 0.4 2.74E+04 10.3

1 4.79E-03 63.1 0.86 0.18 1.17 1.99E-03 1.84E-04 0.44 2.59E-03 110.7

16 7 64.5 2977 3.43 0.57 -0.21 9.49E-03 -2.84E-05 0.4 2.95E+04 12

1 4.83E-03 63.1 1 0.22 1.06 2.02E-03 1.45E-04 0.47 2.57E-03 101.1

16 8 65.1 3173 4.05 0.7 -0.47 9.75E-03 -5.62E-05 0.41 3.18E+04 14.3

1 4.88E-03 63.2 1.16 0.29 1.33 2.05E-03 1.59E-04 0.5 2.54E-03 109.4

16 9 65.7 3375 4.72 0.86 -0.32 9.96E-03 -3.30E-05 0.42 3.41E+04 16.5

1 4.92E-03 63.2 1.34 0.36 1.57 2.07E-03 1.65E-04 0.53 2.52E-03 101.3

16 10 66.3 3179 4.21 0.72 -0.2 9.91E-03 -2.30E-05 0.42 3.24E+04 15.4

1 4.97E-03 63.3 1.18 0.3 1.41 2.04E-03 1.65E-04 0.5 2.49E-03 97.9

16 11 67 2976 3.67 0.59 -0.11 9.77E-03 -1.43E-05 0.41 3.07E+04 13.1

1 5.01E-03 63.3 1.04 0.24 1.22 2.02E-03 1.61E-04 0.47 2.47E-03 95.1

16 12 67.6 2782 3.21 0.48 0.02 9.68E-03 2.74E-06 0.41 2.89E+04 11.4

1 5.06E-03 63.4 0.9 0.2 1.18 1.99E-03 1.78E-04 0.44 2.45E-03 89.1

16 13 68.3 2587 2.79 0.39 0.03 9.65E-03 5.17E-06 0.41 2.72E+04 9.5

1 5.11E-03 63.4 0.79 0.16 0.91 1.99E-03 1.56E-04 0.41 2.42E-03 88.1

16 14 68.9 2393 2.36 0.31 0.02 9.46E-03 3.94E-06 0.4 2.53E+04 7.4

1 5.16E-03 63.5 0.69 0.12 0.74 2.01E-03 1.48E-04 0.37 2.40E-03 88.5

16 15 69.6 2186 2 0.24 -0.05 9.48E-03 -1.26E-05 0.4 2.34E+04 3

1 5.21E-03 63.6 0.58 0.1 0.54 2.02E-03 1.27E-04 0.34 2.38E-03 95.7

16 16 70.2 1993 1.58 0.19 0.06 8.98E-03 1.77E-05 0.36 2.15E+04 NA

54

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 5.25E-03 63.6 0.49 0.07 0.65 2.04E-03 1.83E-04 0.31 2.36E-03 84.5

16 17 70.8 0 0 0 0 0.00E+00 NA

1 5.30E-03 63.6 0.26 0 0 0 2.34E-03

17 1 73 0 0 0 0 0.00E+00 17.3

1 5.45E-03 64.4 0.25 0 0 0 2.27E-03

17 2 60.7 3368 4.26 0.81 -0.8 9.78E-03 -9.09E-05 0.39 3.13E+04 25.7

1 4.53E-03 64.2 1.27 0.32 1.75 2.13E-03 2.00E-04 0.53 2.74E-03 114.5

17 3 56.5 3367 3.9 0.76 -0.91 9.62E-03 -1.12E-04 0.38 2.92E+04 25.5

1 4.23E-03 64 1.19 0.29 1.57 2.14E-03 1.92E-04 0.53 2.94E-03 120.2

17 4 54.1 3367 3.67 0.73 -1.02 9.45E-03 -1.30E-04 0.37 2.79E+04 25.5

1 4.05E-03 63.9 1.15 0.27 1.4 2.16E-03 1.79E-04 0.53 3.07E-03 126

17 5 49.7 3367 3.3 0.69 -1.1 9.27E-03 -1.53E-04 0.35 2.56E+04 34.8

1 3.72E-03 63.8 1.07 0.24 1.13 2.20E-03 1.57E-04 0.53 3.34E-03 134.2

17 6 42.8 3367 2.81 0.61 -1.15 9.15E-03 -1.86E-04 0.34 2.21E+04 35.1

1 3.20E-03 63.5 0.95 0.2 0.97 2.25E-03 1.57E-04 0.53 3.88E-03 139.8

17 7 38.9 3367 2.5 0.54 -1.14 8.98E-03 -2.02E-04 0.33 2.01E+04 34.9

1 2.91E-03 63.2 0.84 0.18 0.74 2.21E-03 1.31E-04 0.53 4.27E-03 147

17 8 35.5 3367 2.25 0.52 -1.21 8.85E-03 -2.35E-04 0.31 1.83E+04 35.3

1 2.66E-03 63 0.8 0.16 0.71 2.31E-03 1.38E-04 0.53 4.68E-03 149.6

17 9 32.5 3367 2.06 0.46 -1.19 8.82E-03 -2.52E-04 0.32 1.68E+04 35.9

1 2.44E-03 62.9 0.72 0.15 0.54 2.24E-03 1.15E-04 0.53 5.10E-03 155.5

17 10 28.5 3367 1.78 0.41 -1.22 8.72E-03 -2.96E-04 0.31 1.47E+04 53.9

1 2.13E-03 62.7 0.64 0.13 0.35 2.29E-03 8.42E-05 0.53 5.84E-03 164.1

17 11 24.2 3368 1.5 0.35 -1.12 8.62E-03 -3.20E-04 0.3 1.25E+04 55.3

1 1.81E-03 62.5 0.55 0.11 0.16 2.30E-03 4.64E-05 0.53 6.87E-03 171.7

17 12 20.7 3368 1.29 0.31 -1.05 8.69E-03 -3.51E-04 0.3 1.07E+04 57.9

1 1.55E-03 62.4 0.48 0.09 -0.01 2.34E-03 -4.35E-06 0.53 8.04E-03 -179.3

17 13 17.8 3368 1.11 0.28 -0.97 8.61E-03 -3.74E-04 0.28 9.18E+03 62.2

1 1.34E-03 62.3 0.44 0.08 -0.17 2.48E-03 -6.41E-05 0.53 9.34E-03 -170.3

17 14 15.5 3368 0.98 0.24 -0.86 8.80E-03 -3.83E-04 0.3 7.97E+03 66.4

1 1.17E-03 62.3 0.37 0.07 -0.28 2.42E-03 -1.24E-04 0.53 1.08E-02 -162.1

17 15 12.4 3368 0.83 0.19 -0.61 9.28E-03 -3.40E-04 0.31 6.34E+03 77.2 55

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 9.30E-04 62.2 0.3 0.06 -0.47 2.49E-03 -2.63E-04 0.53 1.35E-02 -142.3

17 16 10.8 3368 0.75 0.18 -0.42 9.68E-03 -2.70E-04 0.32 5.52E+03 20.6

1 8.12E-04 62.3 0.28 0.06 -0.6 2.59E-03 -3.83E-04 0.53 1.55E-02 -125.1

17 17 11.1 3368 0.79 0.18 -0.26 9.98E-03 -1.63E-04 0.33 5.64E+03 15.5

1 8.30E-04 62.3 0.28 0.06 -0.67 2.61E-03 -4.18E-04 0.53 1.52E-02 -111.3

17 18 11.1 3369 0.83 0.17 -0.13 1.04E-02 -8.22E-05 0.38 5.62E+03 21.2

1 8.30E-04 62.3 0.26 0.06 -0.71 2.40E-03 -4.46E-04 0.53 1.52E-02 -100.4

17 19 11 3369 0.84 0.18 -0.06 1.05E-02 -3.67E-05 0.37 5.60E+03 23.3

1 8.28E-04 62.4 0.27 0.07 -0.73 2.51E-03 -4.56E-04 0.53 1.53E-02 -94.6

17 20 11 2976 0.63 0.11 0.16 1.03E-02 1.27E-04 0.41 4.90E+03 23.8

1 8.22E-04 62.4 0.19 0.04 -0.71 2.22E-03 -5.71E-04 0.47 1.55E-02 -77.4

17 21 10.9 2976 0.63 0.1 0.26 1.03E-02 2.08E-04 0.41 4.88E+03 24.3

1 8.18E-04 62.5 0.18 0.04 -0.69 2.20E-03 -5.63E-04 0.47 1.55E-02 -69.7

17 22 10.9 2976 0.64 0.1 0.29 1.04E-02 2.36E-04 0.42 4.84E+03 24.5

1 8.13E-04 62.5 0.18 0.04 -0.72 2.19E-03 -5.88E-04 0.47 1.56E-02 -68.1

17 23 10.7 0 0 0 0 0.00E+00 18.2

1 8.03E-04 62.5 0.25 0 0 0 1.59E-02

18 1 10.6 0 0 0 0 0.00E+00 18.4

1 7.98E-04 62.6 0.26 0 0 0 1.60E-02

18 2 10.5 1990 0.15 0.04 -0.15 5.60E-03 -2.86E-04 0.12 3.14E+03 20.9

1 7.89E-04 62.6 0.11 0 -0.01 3.03E-03 -2.66E-05 0.31 1.62E-02 -174.7

18 3 10.5 2189 0.27 0.05 -0.31 8.64E-03 -4.86E-04 0.27 3.43E+03 22.3

1 7.85E-04 62.7 0.11 0.01 0.2 2.59E-03 3.19E-04 0.34 1.62E-02 146.7

18 4 10.4 2383 0.38 0.05 -0.34 1.01E-02 -4.50E-04 0.39 3.72E+03 23.5

1 7.81E-04 62.7 0.12 0.02 0.18 2.25E-03 2.35E-04 0.37 1.63E-02 152.5

18 5 10.4 2592 0.43 0.06 -0.26 9.69E-03 -2.87E-04 0.39 4.02E+03 24.2

1 7.77E-04 62.8 0.13 0.02 0.17 2.09E-03 1.95E-04 0.41 1.64E-02 145.9

18 6 10.3 2779 0.45 0.08 -0.15 8.89E-03 -1.50E-04 0.34 4.29E+03 25.4

1 7.74E-04 62.8 0.15 0.03 0.33 2.13E-03 3.25E-04 0.44 1.65E-02 114.8

18 7 10.3 2980 0.51 0.1 -0.07 8.82E-03 -6.38E-05 0.33 4.58E+03 25.8

1 7.70E-04 62.8 0.17 0.03 0.13 2.19E-03 1.09E-04 0.47 1.66E-02 120.4

18 8 10.2 3178 0.65 0.15 -0.1 9.92E-03 -7.67E-05 0.32 4.86E+03 26.1

56

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 7.67E-04 62.9 0.24 0.05 0.1 2.70E-03 7.94E-05 0.5 1.66E-02 134

18 9 10.2 3380 0.72 0.17 0.11 9.73E-03 7.48E-05 0.32 5.15E+03 26.8

1 7.65E-04 62.9 0.26 0.05 0.11 2.56E-03 7.11E-05 0.53 1.67E-02 43.5

18 10 10.2 3176 0.7 0.13 0.18 1.07E-02 1.39E-04 0.39 4.82E+03 26.6

1 7.62E-04 62.9 0.22 0.05 0.04 2.46E-03 2.99E-05 0.5 1.68E-02 12.1

18 11 10.1 2981 0.59 0.1 0.27 1.04E-02 2.33E-04 0.42 4.52E+03 26

1 7.59E-04 63 0.17 0.04 -0.02 2.16E-03 -1.49E-05 0.47 1.68E-02 -3.7

18 12 10.1 2779 0.53 0.07 0.28 1.07E-02 2.83E-04 0.47 4.19E+03 25.5

1 7.56E-04 63 0.14 0.03 0.1 2.06E-03 9.95E-05 0.44 1.69E-02 19.3

18 13 10.1 2586 0.5 0.06 0.25 1.18E-02 2.91E-04 0.55 3.89E+03 24.7

1 7.53E-04 63.1 0.12 0.03 -0.01 2.02E-03 -1.20E-05 0.4 1.69E-02 -2.4

18 14 10 2387 0.48 0.05 0.15 1.33E-02 2.11E-04 0.62 3.57E+03 24.1

1 7.50E-04 63.2 0.11 0.03 -0.24 2.15E-03 -3.24E-04 0.37 1.70E-02 -56.9

18 15 10 2189 0.33 0.04 0.25 1.09E-02 4.17E-04 0.42 3.27E+03 23.7

1 7.49E-04 63.2 0.1 0.02 0.07 2.38E-03 1.20E-04 0.34 1.70E-02 16

18 16 10 1989 0.17 0.03 0.34 6.86E-03 6.70E-04 0.19 2.96E+03 22.8

1 7.46E-04 63.2 0.09 0.01 -0.13 2.59E-03 -2.61E-04 0.31 1.71E-02 -21.3

18 17 10 0 0 0 0 0.00E+00 21.1

1 7.45E-04 63.3 0.24 0 0 0 1.71E-02

19 1 9.8 0 0 0 0 0.00E+00 21.1

1 7.35E-04 63.5 0.25 0 0 0 1.74E-02

19 2 9.8 1989 0.11 0.04 0.17 4.38E-03 3.40E-04 0.09 2.90E+03 23.3

1 7.32E-04 63.6 0.1 0 0 2.91E-03 -7.49E-06 0.31 1.74E-02 -1.3

19 3 9.8 0 0 0 0 0.00E+00 20.9

1 7.31E-04 63.7 0.24 0 0 0 1.74E-02

19 4 9.8 2188 0.26 0.04 -0.09 8.76E-03 -1.59E-04 0.27 3.18E+03 24.4

1 7.29E-04 63.7 0.11 0.01 0.16 2.61E-03 2.70E-04 0.34 1.75E-02 120.6

19 5 9.7 0 0 0 0 0.00E+00 21.9

1 7.28E-04 63.8 0.24 0 0 0 1.75E-02

19 6 9.7 2383 0.32 0.06 -0.05 9.23E-03 -7.78E-05 0.3 3.45E+03 25

1 7.27E-04 63.8 0.12 0.02 -0.32 2.60E-03 -4.60E-04 0.37 1.76E-02 -99.6

19 7 9.7 0 0 0 0 0.00E+00 22 57

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 7.26E-04 63.9 0.26 0 0 0 1.76E-02

19 8 9.7 2587 0.4 0.07 -0.12 9.70E-03 -1.43E-04 0.32 3.74E+03 25.9

1 7.25E-04 63.9 0.15 0.02 -0.08 2.62E-03 -9.25E-05 0.4 1.76E-02 -147.1

19 9 9.7 0 0 0 0 0.00E+00 22.2

1 7.24E-04 64 0.25 0 0 0 1.76E-02

19 10 9.7 2789 0.38 0.08 0.03 7.96E-03 3.50E-05 0.26 4.02E+03 27.2

1 7.22E-04 64 0.15 0.02 0.07 2.33E-03 6.92E-05 0.44 1.77E-02 63.2

19 11 9.6 0 0 0 0 0.00E+00 21.9

1 7.21E-04 64.1 0.24 0 0 0 1.77E-02

19 12 9.6 2977 0.47 0.11 -0.01 8.71E-03 -1.11E-05 0.27 4.28E+03 27.8

1 7.20E-04 64.1 0.19 0.03 -0.03 2.62E-03 -2.38E-05 0.47 1.77E-02 -115

19 13 9.7 0 0 0 0 0.00E+00 NA

1 7.26E-04 64.2 0.25 0 0 0 1.75E-02

19 14 9.8 3179 0.61 0.13 -0.16 9.78E-03 -1.30E-04 0.35 4.66E+03 11.6

1 7.34E-04 64.2 0.21 0.04 0 2.42E-03 -3.35E-06 0.5 1.74E-02 -178.5

19 15 9.9 0 0 0 0 0.00E+00 NA

1 7.39E-04 64.3 0.24 0 0 0 1.72E-02

19 16 10 3373 0.61 0.16 -0.1 8.47E-03 -6.58E-05 0.26 5.03E+03 13.1

1 7.46E-04 64.3 0.25 0.04 0.04 2.58E-03 2.63E-05 0.53 1.71E-02 158.2

19 17 10 0 0 0 0 0.00E+00 NA

1 7.50E-04 64.4 0.24 0 0 0 1.70E-02

20 1 10.5 0 0 0 0 0.00E+00 0

1 7.82E-04 64.7 0.25 0 0 0 1.62E-02

20 2 10.5 1991 0.19 0.04 -0.29 7.05E-03 -5.50E-04 0.16 3.13E+03 9.2

1 7.86E-04 64.8 0.11 0.01 -0.03 3.17E-03 -5.51E-05 0.31 1.62E-02 -174.3

20 3 10.6 0 0 0 0 0.00E+00 0

1 7.89E-04 64.8 0.25 0 0 0 1.61E-02

20 4 10.6 2193 0.24 0.05 -0.01 7.56E-03 -1.50E-05 0.22 3.48E+03 10.6

1 7.91E-04 64.9 0.11 0.01 0.23 2.56E-03 3.62E-04 0.34 1.61E-02 92.4

20 5 10.6 0 0 0 0 0.00E+00 0

1 7.93E-04 64.9 0.24 0 0 0 1.60E-02

20 6 10.6 2391 0.36 0.06 -0.08 9.31E-03 -1.03E-04 0.3 3.81E+03 13.4

58

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 7.95E-04 65 0.14 0.02 -0.17 2.57E-03 -2.23E-04 0.37 1.60E-02 -114.9

20 7 10.7 0 0 0 0 0.00E+00 0

1 7.96E-04 65 0.25 0 0 0 1.59E-02

20 8 10.7 2580 0.38 0.07 -0.05 8.43E-03 -5.50E-05 0.31 4.12E+03 14.5

1 7.97E-04 65 0.13 0.02 -0.01 2.16E-03 -6.45E-06 0.4 1.59E-02 -173.3

20 9 10.7 0 0 0 0 0.00E+00 0

1 7.98E-04 65 0.26 0 0 0 1.59E-02

20 10 10.7 2781 0.4 0.09 -0.03 7.67E-03 -2.75E-05 0.24 4.46E+03 15.5

1 7.99E-04 65.1 0.17 0.02 0.21 2.39E-03 2.00E-04 0.43 1.59E-02 97.8

20 11 10.7 0 0 0 0 0.00E+00 0

1 8.00E-04 65.1 0.25 0 0 0 1.59E-02

20 12 10.7 2981 0.49 0.12 -0.05 8.12E-03 -4.30E-05 0.25 4.79E+03 16.7

1 8.00E-04 65.1 0.21 0.03 0.09 2.51E-03 7.38E-05 0.47 1.58E-02 120.2

20 13 10.7 0 0 0 0 0.00E+00 0

1 8.01E-04 65.2 0.23 0 0 0 1.58E-02

20 14 10.8 3175 0.6 0.14 -0.14 8.82E-03 -1.00E-04 0.29 5.11E+03 17.7

1 8.02E-04 65.2 0.23 0.04 0.1 2.46E-03 7.17E-05 0.5 1.58E-02 144.4

20 15 10.8 0 0 0 0 0.00E+00 0

1 8.03E-04 65.2 0.25 0 0 0 1.58E-02

20 16 10.8 3379 0.66 0.18 -0.1 8.54E-03 -6.11E-05 0.27 5.45E+03 17.7

1 8.04E-04 65.3 0.27 0.05 0.16 2.58E-03 1.00E-04 0.53 1.58E-02 121.4

20 17 10.8 0 0 0 0 0.00E+00 0

1 8.05E-04 65.3 0.25 0 0 0 1.58E-02

21 1 10.8 0 0 0 0 0.00E+00 0

1 8.08E-04 65.6 0.25 0 0 0 1.57E-02

21 2 10.8 1996 0.18 0.04 0.01 6.76E-03 2.16E-05 0.16 3.24E+03 9.8

1 8.07E-04 65.6 0.11 0.01 0.05 3.06E-03 9.97E-05 0.31 1.57E-02 77.8

21 3 10.8 0 0 0 0 0.00E+00 0

1 8.08E-04 65.6 0.26 0 0 0 1.57E-02

21 4 10.8 2190 0.25 0.05 -0.02 7.53E-03 -2.86E-05 0.22 3.56E+03 10.7

1 8.08E-04 65.6 0.12 0.01 0.3 2.62E-03 4.50E-04 0.34 1.57E-02 93.6

21 5 10.8 0 0 0 0 0.00E+00 0 59

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 8.08E-04 65.6 0.25 0 0 0 1.57E-02

21 6 10.8 2388 0.33 0.06 -0.07 8.52E-03 -9.13E-05 0.26 3.88E+03 12.7

1 8.08E-04 65.7 0.14 0.02 -0.08 2.58E-03 -1.07E-04 0.37 1.57E-02 -130.4

21 7 10.8 0 0 0 0 0.00E+00 0

1 8.08E-04 65.7 0.25 0 0 0 1.57E-02

21 8 10.8 2581 0.41 0.07 -0.08 8.95E-03 -8.62E-05 0.32 4.19E+03 13.8

1 8.08E-04 65.7 0.14 0.02 0.02 2.30E-03 1.91E-05 0.4 1.57E-02 167.5

21 9 10.8 0 0 0 0 0.00E+00 0

1 8.08E-04 65.7 0.26 0 0 0 1.57E-02

21 10 10.8 2780 0.39 0.09 -0.02 7.46E-03 -2.17E-05 0.24 4.52E+03 15

1 8.08E-04 65.8 0.17 0.02 0.14 2.31E-03 1.32E-04 0.43 1.57E-02 99.4

21 11 10.8 0 0 0 0 0.00E+00 0

1 8.08E-04 65.8 0.26 0 0 0 1.57E-02

21 12 10.8 2980 0.53 0.11 -0.11 8.72E-03 -8.95E-05 0.29 4.85E+03 16.2

1 8.08E-04 65.8 0.2 0.03 0.03 2.42E-03 2.30E-05 0.47 1.56E-02 165.6

21 13 10.8 0 0 0 0 0.00E+00 0

1 8.08E-04 65.8 0.25 0 0 0 1.57E-02

21 14 10.9 3176 0.64 0.13 -0.17 9.30E-03 -1.21E-04 0.33 5.17E+03 17.7

1 8.08E-04 65.9 0.22 0.04 0.11 2.35E-03 8.20E-05 0.5 1.57E-02 145.9

21 15 10.9 0 0 0 0 0.00E+00 0

1 8.08E-04 65.9 0.25 0 0 0 1.57E-02

22 1 10.9 0 0 0 0 0.00E+00 0

1 8.08E-04 65.9 0.24 0 0 0 1.57E-02

22 2 10.8 3375 0.69 0.17 -0.2 8.83E-03 -1.27E-04 0.3 5.48E+03 18.7

1 8.08E-04 65.9 0.26 0.05 0.22 2.43E-03 1.38E-04 0.53 1.57E-02 132.7

22 3 10.8 3375 0.72 0.17 -0.13 9.19E-03 -8.07E-05 0.3 5.49E+03 18.7

1 8.08E-04 66 0.27 0.05 0.2 2.51E-03 1.26E-04 0.53 1.57E-02 122.7

22 4 10.8 3375 0.72 0.17 -0.02 9.21E-03 -1.40E-05 0.31 5.48E+03 18.9

1 8.08E-04 66 0.26 0.05 0.15 2.45E-03 9.89E-05 0.53 1.57E-02 98.1

22 5 10.8 3375 0.72 0.18 -0.02 9.26E-03 -9.96E-06 0.3 5.49E+03 18.7

1 8.08E-04 66 0.28 0.05 0.12 2.60E-03 7.73E-05 0.53 1.57E-02 97.3

22 6 10.8 3375 0.74 0.18 0.06 9.53E-03 3.77E-05 0.31 5.48E+03 18.6

60

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 8.08E-04 66 0.27 0.06 0.1 2.57E-03 6.22E-05 0.53 1.57E-02 58.7

22 7 10.8 3375 0.75 0.18 0.08 9.70E-03 5.38E-05 0.32 5.48E+03 18.7

1 8.08E-04 66 0.28 0.06 0.08 2.60E-03 4.97E-05 0.53 1.57E-02 42.7

22 8 10.8 3376 0.76 0.16 0.13 9.78E-03 8.30E-05 0.35 5.48E+03 18.7

1 8.06E-04 66.2 0.26 0.06 -0.04 2.41E-03 -2.82E-05 0.53 1.57E-02 -18.7

22 9 10.8 0 0 0 0 0.00E+00 0

1 8.06E-04 66.2 0.23 0 0 0 1.57E-02

23 1 34.2 0 0 0 0 0.00E+00 NA

1 2.54E-03 67.7 0.27 0 0 0 4.90E-03

23 2 35.2 1995 1.13 0.11 -0.54 1.28E-02 -3.07E-04 0.54 1.07E+04 NA

1 2.61E-03 67.7 0.28 0.06 -0.74 2.34E-03 -4.20E-04 0.31 4.77E-03 -126.1

23 3 36 2188 1.31 0.14 -0.59 1.21E-02 -2.70E-04 0.52 1.20E+04 NA

1 2.67E-03 67.8 0.33 0.07 -0.28 2.21E-03 -1.30E-04 0.34 4.66E-03 -154.2

23 4 36.7 2385 1.6 0.17 -0.69 1.22E-02 -2.61E-04 0.56 1.33E+04 NA

1 2.72E-03 67.8 0.37 0.1 -0.36 2.09E-03 -1.38E-04 0.37 4.57E-03 -152.2

23 5 37.2 2583 1.72 0.22 -0.56 1.11E-02 -1.77E-04 0.48 1.46E+04 NA

1 2.76E-03 67.8 0.45 0.11 -0.11 2.10E-03 -3.38E-05 0.4 4.50E-03 -169.2

23 6 37.8 2782 1.9 0.28 -0.44 1.03E-02 -1.19E-04 0.43 1.60E+04 NA

1 2.81E-03 67.8 0.54 0.12 0.25 2.13E-03 6.76E-05 0.43 4.43E-03 150.5

23 7 38.6 2972 2.17 0.35 -0.45 1.01E-02 -1.05E-04 0.42 1.74E+04 NA

1 2.87E-03 67.8 0.61 0.15 0.24 2.09E-03 5.51E-05 0.46 4.34E-03 152.4

23 8 39.2 3177 2.51 0.43 -0.51 1.01E-02 -1.03E-04 0.42 1.89E+04 NA

1 2.91E-03 67.8 0.72 0.18 0.44 2.11E-03 8.83E-05 0.5 4.27E-03 139.4

23 9 39.8 3371 2.79 0.55 -0.38 9.83E-03 -6.59E-05 0.38 2.04E+04 3.1

1 2.95E-03 67.8 0.85 0.21 0.66 2.20E-03 1.15E-04 0.53 4.21E-03 119.8

23 10 44.3 3371 2.99 0.6 -0.32 9.47E-03 -5.06E-05 0.37 2.27E+04 7.3

1 3.29E-03 67.9 0.93 0.22 0.87 2.16E-03 1.36E-04 0.53 3.78E-03 110.4

23 11 45.2 3175 2.73 0.5 -0.14 9.56E-03 -2.48E-05 0.39 2.18E+04 4

1 3.36E-03 67.9 0.82 0.19 0.78 2.10E-03 1.36E-04 0.49 3.70E-03 100.3

23 12 45.8 2980 2.38 0.41 -0.06 9.32E-03 -1.08E-05 0.38 2.08E+04 NA

1 3.40E-03 67.9 0.73 0.15 0.61 2.08E-03 1.18E-04 0.46 3.65E-03 95.2

23 13 46.6 2781 2.08 0.33 0.06 9.18E-03 1.39E-05 0.38 1.97E+04 NA 61

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 3.46E-03 67.9 0.62 0.12 0.78 2.00E-03 1.72E-04 0.43 3.59E-03 85.4

23 14 47.5 2587 1.81 0.27 -0.09 9.06E-03 -2.21E-05 0.38 1.87E+04 NA

1 3.52E-03 67.9 0.54 0.1 0.66 1.98E-03 1.64E-04 0.4 3.52E-03 97.7

23 15 48.2 2389 1.59 0.21 -0.13 9.22E-03 -3.80E-05 0.39 1.75E+04 NA

1 3.58E-03 67.9 0.47 0.08 0.36 1.99E-03 1.04E-04 0.37 3.47E-03 110

23 16 48.8 2188 1.27 0.17 -0.08 8.69E-03 -2.68E-05 0.35 1.62E+04 NA

1 3.62E-03 67.9 0.41 0.06 0.64 2.03E-03 2.16E-04 0.34 3.43E-03 97.1

23 17 49.5 1992 0.98 0.13 -0.02 7.98E-03 -6.90E-06 0.3 1.50E+04 NA

1 3.68E-03 67.9 0.35 0.04 0.32 2.05E-03 1.27E-04 0.31 3.38E-03 93.1

23 18 50.2 0 0 0 0 0.00E+00 NA

1 3.73E-03 68 0.26 0 0 0 3.33E-03

24 1 50.2 0 0 0 0 0.00E+00 NA

1 3.73E-03 68 0.26 0 0 0 3.33E-03

24 2 51.2 1991 0.97 0.14 0.16 7.64E-03 6.19E-05 0.28 1.55E+04 NA

1 3.80E-03 68 0.37 0.04 0.3 2.10E-03 1.16E-04 0.31 3.27E-03 61.9

24 3 51.9 2188 1.29 0.18 0.04 8.25E-03 1.25E-05 0.32 1.73E+04 NA

1 3.85E-03 68 0.44 0.06 0.65 2.04E-03 2.08E-04 0.34 3.22E-03 86.6

24 4 52.8 2384 1.62 0.23 -0.07 8.62E-03 -1.83E-05 0.35 1.92E+04 NA

1 3.92E-03 68 0.51 0.08 0.54 2.00E-03 1.44E-04 0.37 3.17E-03 97.3

24 5 53.5 2584 1.9 0.3 -0.18 8.49E-03 -4.04E-05 0.34 2.10E+04 NA

1 3.97E-03 68.1 0.61 0.1 0.93 1.98E-03 2.05E-04 0.4 3.13E-03 101.1

24 6 54.1 2780 2.24 0.39 -0.18 8.55E-03 -3.37E-05 0.33 2.29E+04 NA

1 4.01E-03 68.1 0.74 0.13 1.25 2.05E-03 2.37E-04 0.43 3.09E-03 98.1

24 7 54.7 2978 2.67 0.48 -0.47 8.78E-03 -7.60E-05 0.35 2.48E+04 6.9

1 4.06E-03 68.1 0.86 0.17 1.52 2.05E-03 2.49E-04 0.46 3.05E-03 107

24 8 55.4 3174 3.18 0.6 -0.29 9.09E-03 -4.15E-05 0.36 2.68E+04 9.6

1 4.11E-03 68.1 0.99 0.22 1.37 2.07E-03 1.94E-04 0.49 3.02E-03 102.1

24 9 56.1 3373 3.65 0.75 -0.36 9.11E-03 -4.52E-05 0.35 2.88E+04 11.4

1 4.16E-03 68.1 1.17 0.27 1.46 2.13E-03 1.82E-04 0.53 2.98E-03 104

24 10 56.8 3172 3.27 0.61 -0.3 9.11E-03 -4.19E-05 0.37 2.75E+04 9.6

1 4.22E-03 68.1 1.01 0.22 1.34 2.06E-03 1.86E-04 0.49 2.94E-03 102.7

24 11 57.8 2977 2.81 0.51 -0.52 8.73E-03 -8.06E-05 0.35 2.62E+04 5.9

62

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 4.29E-03 68.1 0.89 0.18 1.25 2.03E-03 1.94E-04 0.46 2.89E-03 112.6

24 12 58.6 2778 2.45 0.41 -0.32 8.65E-03 -5.66E-05 0.35 2.48E+04 3

1 4.34E-03 68.1 0.77 0.14 1.18 1.99E-03 2.07E-04 0.43 2.85E-03 105.3

24 13 59.3 2581 2.11 0.33 -0.47 8.52E-03 -9.33E-05 0.34 2.33E+04 NA

1 4.40E-03 68.1 0.67 0.11 0.98 1.98E-03 1.96E-04 0.4 2.82E-03 115.4

24 14 59.9 2385 1.84 0.26 -0.41 8.58E-03 -9.56E-05 0.35 2.18E+04 NA

1 4.44E-03 68.2 0.58 0.09 0.7 1.99E-03 1.64E-04 0.37 2.79E-03 120.3

24 15 60.6 2191 1.47 0.21 -0.5 8.03E-03 -1.37E-04 0.31 2.02E+04 NA

1 4.49E-03 68.2 0.5 0.06 0.9 2.02E-03 2.44E-04 0.34 2.76E-03 119.3

24 16 61.2 1994 1.15 0.16 -0.46 7.52E-03 -1.50E-04 0.27 1.86E+04 NA

1 4.54E-03 68.2 0.43 0.04 0.6 2.06E-03 1.95E-04 0.31 2.73E-03 127.6

24 17 61.9 0 -0.1 0 -0.5 0.00E+00 NA

1 4.59E-03 68.2 0.24 0 0.08 0 2.70E-03 -9.5

25 1 71 0 0.02 0 0.19 0.00E+00 NA

1 5.27E-03 68.5 0.26 0 0.04 0 2.35E-03 11.3

25 2 72.2 1992 1.58 0.2 0.25 8.79E-03 6.81E-05 0.33 2.19E+04 NA

1 5.35E-03 68.5 0.54 0.07 0.9 2.18E-03 2.48E-04 0.31 2.31E-03 74.7

25 3 73 2193 2 0.27 -0.02 9.09E-03 -4.99E-06 0.35 2.44E+04 NA

1 5.41E-03 68.5 0.64 0.09 1.29 2.13E-03 2.91E-04 0.34 2.29E-03 91

25 4 74.1 2387 2.48 0.35 -0.29 9.36E-03 -5.38E-05 0.36 2.70E+04 NA

1 5.49E-03 68.5 0.78 0.13 1.29 2.15E-03 2.43E-04 0.37 2.25E-03 102.5

25 5 74.8 2585 2.94 0.44 -0.37 9.37E-03 -5.83E-05 0.38 2.95E+04 3.9

1 5.54E-03 68.6 0.88 0.17 1.46 2.07E-03 2.32E-04 0.4 2.23E-03 104.1

25 6 75.5 2782 3.48 0.55 -0.49 9.49E-03 -6.70E-05 0.39 3.20E+04 7.9

1 5.60E-03 68.6 1.04 0.21 1.87 2.07E-03 2.54E-04 0.43 2.21E-03 104.8

25 7 77.5 2979 4.09 0.69 -0.67 9.50E-03 -7.75E-05 0.39 3.52E+04 11.4

1 5.74E-03 68.6 1.21 0.27 1.97 2.06E-03 2.27E-04 0.46 2.16E-03 108.8

25 8 76.9 3177 4.82 0.85 -1.11 9.92E-03 -1.13E-04 0.41 3.72E+04 13.7

1 5.70E-03 68.6 1.4 0.34 1.99 2.10E-03 2.03E-04 0.49 2.17E-03 119.1

25 9 79.7 3177 5.07 0.88 -1.2 1.01E-02 -1.19E-04 0.41 3.86E+04 14.2

1 5.90E-03 68.6 1.46 0.36 1.97 2.11E-03 1.94E-04 0.49 2.10E-03 121.4

25 10 80.4 3371 5.78 1.1 -1.24 1.01E-02 -1.08E-04 0.4 4.13E+04 16.2 63

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 5.95E-03 68.6 1.71 0.44 2.19 2.19E-03 1.91E-04 0.53 2.08E-03 119.6

25 11 81.1 3173 5.18 0.89 -1.13 1.01E-02 -1.10E-04 0.42 3.92E+04 13.9

1 6.01E-03 68.6 1.48 0.37 1.91 2.11E-03 1.85E-04 0.49 2.06E-03 120.7

25 12 81.7 2978 4.53 0.74 -1.28 9.98E-03 -1.40E-04 0.41 3.71E+04 12.2

1 6.06E-03 68.7 1.31 0.3 1.78 2.10E-03 1.95E-04 0.46 2.04E-03 125.7

25 13 82.5 2782 3.91 0.6 -0.7 9.78E-03 -8.74E-05 0.4 3.50E+04 9.4

1 6.11E-03 68.7 1.13 0.24 1.55 2.07E-03 1.93E-04 0.43 2.02E-03 114.4

25 14 83.1 2583 3.34 0.48 -0.63 9.62E-03 -8.95E-05 0.4 3.27E+04 6

1 6.16E-03 68.7 0.98 0.19 1.23 2.06E-03 1.76E-04 0.4 2.01E-03 117

25 15 83.7 2382 2.84 0.38 -0.55 9.53E-03 -9.25E-05 0.39 3.04E+04 NA

1 6.20E-03 68.7 0.84 0.15 0.89 2.07E-03 1.49E-04 0.37 1.99E-03 121.8

25 16 84.3 2188 2.32 0.3 -0.41 9.17E-03 -8.01E-05 0.36 2.81E+04 NA

1 6.25E-03 68.7 0.73 0.11 1.09 2.10E-03 2.15E-04 0.34 1.98E-03 110.5

25 17 85.2 1990 1.87 0.23 -0.08 8.85E-03 -1.79E-05 0.34 2.58E+04 NA

1 6.31E-03 68.7 0.62 0.08 0.72 2.14E-03 1.69E-04 0.31 1.96E-03 96

25 18 86.3 0 0 0 0 0.00E+00 NA

1 6.39E-03 68.8 0.26 0 0 0 1.94E-03

26 1 86.3 0 0 0 0 0.00E+00 NA

1 6.39E-03 68.8 0.26 0 0 0 1.94E-03

26 2 87.7 1991 1.96 0.25 0.19 9.02E-03 4.37E-05 0.34 2.66E+04 NA

1 6.50E-03 68.8 0.65 0.08 0.66 2.19E-03 1.49E-04 0.31 1.90E-03 73.7

26 3 88.5 2190 2.52 0.32 -0.11 9.46E-03 -2.01E-05 0.38 2.95E+04 NA

1 6.55E-03 68.8 0.77 0.12 1.11 2.12E-03 2.07E-04 0.34 1.89E-03 95.5

26 4 89.7 2388 3.15 0.42 -0.44 9.84E-03 -6.81E-05 0.4 3.26E+04 NA

1 6.64E-03 68.9 0.93 0.17 0.98 2.12E-03 1.52E-04 0.37 1.86E-03 114.2

26 5 90.5 2584 3.71 0.53 -0.6 9.81E-03 -7.82E-05 0.41 3.57E+04 7.7

1 6.70E-03 68.9 1.07 0.21 1.39 2.07E-03 1.82E-04 0.4 1.85E-03 113.3

26 6 91.1 2781 4.46 0.67 -1.06 1.01E-02 -1.20E-04 0.42 3.86E+04 10.4

1 6.75E-03 68.9 1.26 0.28 1.68 2.08E-03 1.89E-04 0.43 1.83E-03 122.4

26 7 91.9 2974 5.18 0.83 -1.21 1.02E-02 -1.18E-04 0.42 4.16E+04 12.9

1 6.80E-03 68.9 1.46 0.35 1.72 2.10E-03 1.67E-04 0.46 1.82E-03 125.1

26 8 92.5 3172 6.12 1.03 -1.58 1.05E-02 -1.34E-04 0.44 4.47E+04 15.6

64

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 6.85E-03 68.9 1.7 0.45 2.05 2.13E-03 1.74E-04 0.49 1.81E-03 127.6

26 9 93.2 3374 7.03 1.26 -1.67 1.06E-02 -1.25E-04 0.44 4.79E+04 17.1

1 6.90E-03 68.9 1.96 0.55 2.22 2.16E-03 1.66E-04 0.53 1.79E-03 126.9

26 10 93.9 3173 6.26 1.04 -1.44 1.06E-02 -1.21E-04 0.44 4.54E+04 15

1 6.95E-03 68.9 1.72 0.46 1.99 2.13E-03 1.67E-04 0.49 1.78E-03 125.9

26 11 94.5 2974 5.44 0.85 -1.06 1.04E-02 -1.00E-04 0.44 4.28E+04 12.8

1 7.00E-03 69 1.5 0.37 1.68 2.10E-03 1.59E-04 0.46 1.77E-03 122.2

26 12 95.3 2778 4.76 0.7 -1.08 1.03E-02 -1.17E-04 0.44 4.03E+04 10.4

1 7.06E-03 69 1.31 0.3 1.43 2.09E-03 1.54E-04 0.43 1.75E-03 127.2

26 13 95.9 2582 4.03 0.56 -0.68 1.01E-02 -8.43E-05 0.42 3.77E+04 7.5

1 7.10E-03 69 1.13 0.24 1.24 2.07E-03 1.54E-04 0.4 1.74E-03 118.7

26 14 96.7 2384 3.48 0.45 -0.76 1.01E-02 -1.09E-04 0.42 3.51E+04 4.2

1 7.16E-03 69 0.99 0.19 0.97 2.10E-03 1.40E-04 0.37 1.73E-03 128.1

26 15 97.4 2188 2.87 0.35 -0.53 9.82E-03 -8.97E-05 0.4 3.25E+04 NA

1 7.21E-03 69 0.84 0.14 1.1 2.11E-03 1.88E-04 0.34 1.72E-03 115.6

26 16 98 1988 2.28 0.27 -0.38 9.41E-03 -7.77E-05 0.37 2.97E+04 NA

1 7.25E-03 69 0.71 0.1 0.77 2.13E-03 1.59E-04 0.31 1.71E-03 116.1

26 17 98.6 0 0 0 0 0.00E+00 NA

1 7.30E-03 69.1 0.26 0 0 0 1.69E-03

27 1 98.6 0 0 0 0 0.00E+00 NA

1 7.30E-03 69.1 0.26 0 0 0 1.69E-03

27 2 99.7 1990 2.36 0.28 -0.15 9.54E-03 -3.08E-05 0.37 3.02E+04 NA

1 7.38E-03 69.1 0.74 0.1 0.8 2.18E-03 1.61E-04 0.31 1.67E-03 100.8

27 3 100.6 2186 3.02 0.37 -0.21 1.00E-02 -3.43E-05 0.4 3.35E+04 NA

1 7.45E-03 69.1 0.89 0.15 1.25 2.16E-03 2.06E-04 0.34 1.66E-03 99.5

27 4 101.6 2384 3.72 0.48 -0.51 1.03E-02 -7.01E-05 0.43 3.69E+04 4.1

1 7.52E-03 69.1 1.05 0.2 1.27 2.12E-03 1.75E-04 0.37 1.64E-03 111.8

27 5 102.3 2583 4.45 0.61 -0.7 1.04E-02 -8.10E-05 0.44 4.02E+04 8.4

1 7.57E-03 69.1 1.23 0.26 1.5 2.11E-03 1.74E-04 0.4 1.63E-03 114.9

27 6 102.9 2780 5.29 0.77 -1.25 1.06E-02 -1.25E-04 0.45 4.36E+04 11.5

1 7.61E-03 69.2 1.45 0.34 1.81 2.13E-03 1.81E-04 0.43 1.62E-03 124.6

27 7 103.5 2977 6.12 0.93 -0.94 1.07E-02 -8.12E-05 0.45 4.69E+04 13.7 65

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 7.66E-03 69.2 1.65 0.42 1.55 2.10E-03 1.34E-04 0.46 1.61E-03 121.1

27 8 104.2 3181 7.26 1.17 -1.97 1.10E-02 -1.48E-04 0.47 5.05E+04 15.9

1 7.71E-03 69.2 1.92 0.55 2.18 2.13E-03 1.64E-04 0.5 1.60E-03 132.1

27 9 104.8 3372 8.26 1.42 -2.19 1.11E-02 -1.46E-04 0.46 5.39E+04 18.2

1 7.76E-03 69.2 2.22 0.66 2.41 2.17E-03 1.60E-04 0.53 1.59E-03 132.2

27 10 105.6 3172 7.36 1.16 -2.02 1.11E-02 -1.51E-04 0.48 5.10E+04 15.9

1 7.82E-03 69.2 1.93 0.55 2.17 2.12E-03 1.62E-04 0.49 1.58E-03 132.9

27 11 106.4 2978 6.4 0.95 -1.79 1.08E-02 -1.51E-04 0.47 4.83E+04 13.9

1 7.87E-03 69.3 1.67 0.45 1.87 2.07E-03 1.58E-04 0.46 1.57E-03 133.7

27 12 107 2779 5.53 0.77 -1.5 1.07E-02 -1.44E-04 0.46 4.53E+04 11.5

1 7.92E-03 69.3 1.46 0.36 1.79 2.06E-03 1.72E-04 0.43 1.56E-03 129.8

27 13 107.5 2580 4.72 0.62 -1.32 1.05E-02 -1.46E-04 0.45 4.23E+04 8.4

1 7.96E-03 69.3 1.26 0.28 1.49 2.06E-03 1.65E-04 0.4 1.55E-03 131.5

27 14 108.2 2383 4.03 0.49 -1.01 1.05E-02 -1.30E-04 0.45 3.93E+04 6

1 8.00E-03 69.3 1.09 0.22 1.1 2.06E-03 1.42E-04 0.37 1.55E-03 132.4

27 15 108.8 2187 3.32 0.39 -0.74 1.02E-02 -1.13E-04 0.42 3.63E+04 NA

1 8.05E-03 69.3 0.94 0.17 1.16 2.10E-03 1.77E-04 0.34 1.54E-03 122.6

27 16 109.3 1993 2.68 0.3 -0.54 9.84E-03 -9.82E-05 0.39 3.32E+04 NA

1 8.09E-03 69.4 0.8 0.12 0.81 2.14E-03 1.48E-04 0.31 1.53E-03 123.6

27 17 109.9 0 0 0 0 0.00E+00 NA

1 8.13E-03 69.4 0.26 0 0 0 1.52E-03

28 1 109.9 0 0 0 0 0.00E+00 NA

1 8.13E-03 69.4 0.26 0 0 0 1.52E-03

28 2 111 1990 2.75 0.31 -0.35 9.98E-03 -6.32E-05 0.4 3.36E+04 NA

1 8.21E-03 69.4 0.82 0.12 0.87 2.18E-03 1.58E-04 0.31 1.51E-03 111.8

28 3 111.6 2191 3.52 0.41 -0.51 1.05E-02 -7.59E-05 0.44 3.72E+04 NA

1 8.26E-03 69.4 0.98 0.18 1.29 2.13E-03 1.91E-04 0.34 1.50E-03 111.7

28 4 112.3 2387 4.3 0.53 -0.9 1.07E-02 -1.12E-04 0.45 4.08E+04 6.3

1 8.31E-03 69.4 1.16 0.24 1.25 2.12E-03 1.55E-04 0.37 1.49E-03 125.8

28 5 112.9 2582 5.11 0.65 -1.27 1.08E-02 -1.34E-04 0.48 4.44E+04 9.4

1 8.35E-03 69.4 1.31 0.31 1.65 2.04E-03 1.74E-04 0.4 1.48E-03 127.6

28 6 113.5 2780 6.01 0.82 -1.62 1.09E-02 -1.47E-04 0.48 4.81E+04 12

66

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 8.40E-03 69.4 1.54 0.39 2.01 2.05E-03 1.82E-04 0.43 1.47E-03 128.9

28 7 114.1 2976 7.02 1.01 -2.37 1.11E-02 -1.86E-04 0.49 5.17E+04 15

1 8.44E-03 69.5 1.78 0.5 2.36 2.06E-03 1.86E-04 0.46 1.46E-03 135.1

28 8 114.8 3175 8.21 1.28 -2.75 1.13E-02 -1.89E-04 0.49 5.55E+04 16.7

1 8.49E-03 69.5 2.12 0.63 2.71 2.14E-03 1.86E-04 0.49 1.46E-03 135.4

28 9 115.3 3371 9.38 1.55 -2.99 1.14E-02 -1.81E-04 0.49 5.92E+04 18.5

1 8.53E-03 69.5 2.41 0.76 2.84 2.15E-03 1.72E-04 0.52 1.45E-03 136.5

28 10 115.9 3173 8.33 1.26 -2.4 1.14E-02 -1.63E-04 0.51 5.60E+04 16.6

1 8.58E-03 69.5 2.08 0.64 2.6 2.09E-03 1.77E-04 0.49 1.44E-03 132.6

28 11 116.6 2979 7.28 1.04 -2.27 1.12E-02 -1.74E-04 0.5 5.29E+04 14.2

1 8.62E-03 69.6 1.84 0.52 2.26 2.07E-03 1.73E-04 0.46 1.43E-03 135.1

28 12 117.3 2780 6.25 0.83 -1.65 1.10E-02 -1.45E-04 0.49 4.96E+04 12

1 8.67E-03 69.6 1.57 0.41 2.35 2.03E-03 2.06E-04 0.43 1.43E-03 125.2

28 13 117.9 2584 5.39 0.67 -1.73 1.09E-02 -1.74E-04 0.49 4.64E+04 9.7

1 8.72E-03 69.6 1.36 0.33 1.68 2.02E-03 1.69E-04 0.4 1.42E-03 135.9

28 14 118.6 2385 4.61 0.54 -1.69 1.09E-02 -1.99E-04 0.48 4.31E+04 6.3

1 8.77E-03 69.6 1.19 0.26 1.37 2.07E-03 1.62E-04 0.37 1.41E-03 141

28 15 119.3 2188 3.79 0.43 -1.02 1.06E-02 -1.41E-04 0.45 3.97E+04 NA

1 8.82E-03 69.7 1.04 0.19 1.27 2.12E-03 1.77E-04 0.34 1.40E-03 128.6

28 16 119.9 1992 3.06 0.32 -0.72 1.03E-02 -1.20E-04 0.43 3.64E+04 NA

1 8.86E-03 69.7 0.85 0.14 0.99 2.08E-03 1.66E-04 0.31 1.40E-03 125.8

28 17 120.4 0 0 0 0 0.00E+00 NA

1 8.90E-03 69.7 0.26 0 0 0 1.39E-03

29 1 120.4 0 0 0 0 0.00E+00 NA

1 8.90E-03 69.7 0.26 0 0 0 1.39E-03

29 2 121.4 1990 3.2 0.34 -0.27 1.06E-02 -4.53E-05 0.44 3.68E+04 NA

1 8.98E-03 69.7 0.89 0.15 1.22 2.16E-03 2.02E-04 0.31 1.38E-03 102.6

29 3 122 2186 3.98 0.45 -0.77 1.09E-02 -1.04E-04 0.46 4.06E+04 0.3

1 9.02E-03 69.7 1.07 0.21 1.47 2.15E-03 2.00E-04 0.34 1.37E-03 117.5

29 4 122.8 2387 4.87 0.56 -1.26 1.11E-02 -1.43E-04 0.5 4.46E+04 6.8

1 9.08E-03 69.7 1.23 0.28 1.47 2.05E-03 1.67E-04 0.37 1.36E-03 130.5

29 5 123.4 2581 5.77 0.7 -1.78 1.12E-02 -1.72E-04 0.51 4.85E+04 10.3 67

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 9.12E-03 69.7 1.43 0.36 1.92 2.03E-03 1.86E-04 0.4 1.36E-03 132.7

29 6 124 2782 6.82 0.89 -2.28 1.14E-02 -1.89E-04 0.51 5.25E+04 12.8

1 9.17E-03 69.7 1.68 0.46 2.26 2.05E-03 1.87E-04 0.43 1.35E-03 135.2

29 7 124.7 2977 7.96 1.13 -2.72 1.15E-02 -1.95E-04 0.51 5.65E+04 14.8

1 9.22E-03 69.7 1.99 0.57 2.42 2.11E-03 1.74E-04 0.46 1.34E-03 138.2

29 8 125.5 3176 9.26 1.4 -3.22 1.17E-02 -2.02E-04 0.51 6.07E+04 17.1

1 9.28E-03 69.8 2.31 0.72 3 2.13E-03 1.88E-04 0.49 1.33E-03 137

29 9 126.3 3371 10.61 1.68 -3.5 1.18E-02 -1.94E-04 0.52 6.48E+04 18.9

1 9.34E-03 69.8 2.62 0.88 3.03 2.14E-03 1.68E-04 0.52 1.32E-03 139.1

29 10 126.9 3173 9.4 1.38 -3.07 1.18E-02 -1.91E-04 0.53 6.13E+04 16.7

1 9.38E-03 69.8 2.29 0.73 2.73 2.09E-03 1.70E-04 0.49 1.32E-03 138.3

29 11 127.6 2979 8.24 1.14 -2.74 1.16E-02 -1.92E-04 0.53 5.79E+04 15

1 9.43E-03 69.8 2 0.6 2.45 2.07E-03 1.72E-04 0.46 1.31E-03 138.2

29 12 128.1 2779 7.06 0.92 -2.31 1.14E-02 -1.86E-04 0.52 5.42E+04 12.9

1 9.47E-03 69.8 1.73 0.47 2.11 2.05E-03 1.70E-04 0.43 1.31E-03 137.6

29 13 128.8 2585 6.09 0.74 -2.07 1.13E-02 -1.91E-04 0.51 5.07E+04 10.1

1 9.52E-03 69.8 1.5 0.38 1.62 2.04E-03 1.50E-04 0.4 1.30E-03 141.9

29 14 129.4 2385 5.16 0.59 -1.18 1.12E-02 -1.28E-04 0.5 4.70E+04 7.1

1 9.57E-03 69.9 1.29 0.29 1 2.05E-03 1.08E-04 0.37 1.29E-03 139.7

29 15 130.1 2187 4.24 0.46 -1.28 1.09E-02 -1.64E-04 0.47 4.33E+04 NA

1 9.62E-03 69.9 1.11 0.22 1.2 2.09E-03 1.53E-04 0.34 1.29E-03 136.9

29 16 130.9 1989 3.41 0.35 -0.99 1.06E-02 -1.52E-04 0.45 3.96E+04 NA

1 9.67E-03 69.9 0.93 0.16 0.95 2.10E-03 1.46E-04 0.31 1.28E-03 136.1

29 17 131.7 0 0 0 0 0.00E+00 NA

1 9.73E-03 69.9 0.27 0 0 0 1.27E-03

30 1 131.7 0 0 0 0 0.00E+00 NA

1 9.73E-03 69.9 0.27 0 0 0 1.27E-03

30 2 132.8 1990 3.61 0.38 -0.43 1.10E-02 -6.55E-05 0.44 4.02E+04 NA

1 9.82E-03 69.9 1.01 0.17 1.13 2.24E-03 1.70E-04 0.31 1.26E-03 111.1

30 3 133.5 2189 4.52 0.48 -1.07 1.13E-02 -1.34E-04 0.49 4.45E+04 NA

1 9.87E-03 69.9 1.16 0.24 1.49 2.12E-03 1.86E-04 0.34 1.25E-03 125.7

30 4 134.1 2385 5.45 0.61 -1.23 1.14E-02 -1.28E-04 0.52 4.87E+04 7.4

68

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 9.91E-03 69.9 1.34 0.31 1.66 2.05E-03 1.74E-04 0.37 1.25E-03 126.4

30 5 134.6 2584 6.49 0.78 -1.85 1.15E-02 -1.63E-04 0.52 5.29E+04 10.3

1 9.95E-03 70 1.59 0.41 2.09 2.07E-03 1.85E-04 0.4 1.24E-03 131.4

30 6 135.2 2780 7.65 0.99 -2.44 1.17E-02 -1.86E-04 0.52 5.72E+04 13.1

1 9.99E-03 70 1.88 0.52 2.41 2.10E-03 1.83E-04 0.43 1.24E-03 135.4

30 7 135.8 2976 8.91 1.22 -3.13 1.18E-02 -2.07E-04 0.53 6.15E+04 15.5

1 1.00E-02 70 2.15 0.65 2.87 2.09E-03 1.89E-04 0.46 1.23E-03 137.5

30 8 136.4 3172 10.32 1.5 -3.5 1.20E-02 -2.02E-04 0.54 6.59E+04 17.4

1 1.01E-02 70 2.49 0.81 3.22 2.12E-03 1.87E-04 0.49 1.23E-03 137.3

30 9 137.1 3372 11.77 1.84 -3.82 1.21E-02 -1.95E-04 0.54 7.04E+04 19.2

1 1.01E-02 70 2.86 0.98 3.91 2.15E-03 1.99E-04 0.52 1.22E-03 134.3

30 10 137.8 3177 10.44 1.51 -3.57 1.20E-02 -2.04E-04 0.54 6.66E+04 17.3

1 1.02E-02 70 2.5 0.82 3.38 2.10E-03 1.93E-04 0.49 1.21E-03 136.6

30 11 138.4 2975 9.13 1.23 -3.09 1.19E-02 -2.00E-04 0.54 6.27E+04 15.1

1 1.02E-02 70 2.18 0.67 2.85 2.08E-03 1.85E-04 0.46 1.21E-03 137.3

30 12 139.2 2780 7.88 0.99 -2.52 1.17E-02 -1.86E-04 0.54 5.89E+04 13.1

1 1.03E-02 70 1.88 0.54 2.47 2.04E-03 1.83E-04 0.43 1.20E-03 135.5

30 13 139.8 2581 6.74 0.79 -2.28 1.16E-02 -1.95E-04 0.53 5.49E+04 10.2

1 1.03E-02 70 1.61 0.42 2.09 2.03E-03 1.78E-04 0.4 1.20E-03 137.5

30 14 140.5 2386 5.75 0.63 -2.01 1.15E-02 -1.99E-04 0.53 5.10E+04 8.1

1 1.04E-02 70.1 1.39 0.33 1.65 2.03E-03 1.64E-04 0.37 1.19E-03 140.5

30 15 141.1 2188 4.76 0.49 -1.54 1.13E-02 -1.82E-04 0.5 4.70E+04 3.2

1 1.04E-02 70.1 1.19 0.25 1.46 2.06E-03 1.72E-04 0.34 1.19E-03 136.6

30 16 141.8 1992 3.85 0.38 -1.36 1.09E-02 -1.93E-04 0.47 4.30E+04 NA

1 1.05E-02 70.1 1.01 0.18 1.19 2.09E-03 1.68E-04 0.31 1.18E-03 139

30 17 142.6 0 0 0 0 0.00E+00 NA

1 1.05E-02 70.1 0.26 0 0 0 1.17E-03

31 1 142.6 0 0 0 0 0.00E+00 NA

1 1.05E-02 70.1 0.26 0 0 0 1.17E-03

31 2 143.8 1993 4.01 0.41 -0.73 1.12E-02 -1.02E-04 0.47 4.36E+04 NA

1 1.06E-02 70.1 1.07 0.19 1.42 2.19E-03 1.98E-04 0.31 1.16E-03 117.2

31 3 145.1 2188 4.94 0.51 -1.03 1.14E-02 -1.18E-04 0.51 4.83E+04 2.1

69

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 1.07E-02 70.1 1.23 0.26 2.11 2.08E-03 2.41E-04 0.34 1.15E-03 116.1

31 4 146 2385 6.02 0.68 -1.46 1.16E-02 -1.40E-04 0.51 5.30E+04 7.6

1 1.08E-02 70.2 1.49 0.35 2.19 2.10E-03 2.10E-04 0.37 1.15E-03 123.7

31 5 146.7 2582 7.2 0.85 -2.32 1.18E-02 -1.89E-04 0.54 5.77E+04 11.1

1 1.08E-02 70.2 1.73 0.46 2.64 2.07E-03 2.15E-04 0.4 1.14E-03 131.3

31 6 147.6 2779 8.46 1.06 -2.83 1.19E-02 -1.97E-04 0.55 6.24E+04 13.5

1 1.09E-02 70.2 2 0.58 2.95 2.05E-03 2.06E-04 0.43 1.13E-03 133.8

31 7 148.5 2979 9.85 1.32 -3.26 1.20E-02 -1.97E-04 0.55 6.73E+04 15.4

1 1.10E-02 70.2 2.33 0.72 3.61 2.07E-03 2.18E-04 0.46 1.13E-03 132.1

31 8 149.3 3171 11.48 1.63 -4.21 1.22E-02 -2.23E-04 0.56 7.20E+04 17.9

1 1.10E-02 70.2 2.7 0.91 3.28 2.10E-03 1.74E-04 0.49 1.12E-03 142.1

31 9 150.1 3371 13.04 1.99 -4.56 1.22E-02 -2.13E-04 0.55 7.70E+04 19.5

1 1.11E-02 70.2 3.1 1.1 4.04 2.13E-03 1.89E-04 0.52 1.11E-03 138.4

31 10 150.8 3173 11.58 1.65 -4 1.22E-02 -2.10E-04 0.56 7.28E+04 17.9

1 1.11E-02 70.2 2.72 0.92 3.23 2.10E-03 1.69E-04 0.49 1.11E-03 141.1

31 11 151.4 2976 10.05 1.33 -3.07 1.20E-02 -1.82E-04 0.55 6.85E+04 15.8

1 1.12E-02 70.2 2.35 0.74 2.74 2.05E-03 1.62E-04 0.46 1.11E-03 138.3

31 12 152 2777 8.7 1.07 -2.9 1.19E-02 -1.97E-04 0.55 6.42E+04 13.2

1 1.12E-02 70.3 2.03 0.59 2.46 2.03E-03 1.67E-04 0.43 1.10E-03 139.7

31 13 152.8 2581 7.49 0.87 -2.84 1.18E-02 -2.22E-04 0.55 6.00E+04 11.5

1 1.13E-02 70.3 1.77 0.47 1.86 2.03E-03 1.46E-04 0.4 1.10E-03 146.7

31 14 153.3 2385 6.35 0.69 -2.24 1.17E-02 -2.05E-04 0.54 5.56E+04 7.5

1 1.13E-02 70.3 1.52 0.37 1.36 2.04E-03 1.24E-04 0.37 1.09E-03 148.7

31 15 153.8 2186 5.25 0.54 -1.83 1.14E-02 -1.99E-04 0.52 5.11E+04 2.9

1 1.14E-02 70.3 1.29 0.28 1.34 2.05E-03 1.45E-04 0.34 1.09E-03 143.9

31 16 154.6 1996 4.27 0.42 -1.37 1.11E-02 -1.77E-04 0.48 4.69E+04 NA

1 1.14E-02 70.3 1.1 0.2 0.91 2.09E-03 1.17E-04 0.31 1.08E-03 146.4

31 17 155.3 0 0 0 0 0.00E+00 NA

1 1.15E-02 70.3 0.28 0 0 0 1.08E-03

32 1 155.3 0 0 0 0 0.00E+00 NA

1 1.15E-02 70.3 0.28 0 0 0 1.08E-03

32 2 156.4 1994 4.34 0.43 -0.83 1.12E-02 -1.07E-04 0.48 4.74E+04 NA

70

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 1.15E-02 70.4 1.14 0.21 1.17 2.14E-03 1.50E-04 0.31 1.07E-03 125.5

32 3 157.2 2188 5.41 0.56 -1.69 1.15E-02 -1.79E-04 0.51 5.23E+04 4.4

1 1.16E-02 70.4 1.34 0.29 1.62 2.08E-03 1.71E-04 0.34 1.06E-03 136.3

32 4 157.8 2385 6.54 0.71 -2.26 1.17E-02 -2.00E-04 0.53 5.73E+04 8.7

1 1.17E-02 70.4 1.57 0.38 1.84 2.05E-03 1.63E-04 0.37 1.06E-03 140.8

32 5 158.5 2580 7.67 0.9 -2.57 1.16E-02 -1.94E-04 0.54 6.22E+04 10.8

1 1.17E-02 70.4 1.83 0.48 2.45 2.03E-03 1.85E-04 0.4 1.06E-03 136.4

32 6 159 2779 9.12 1.15 -3.39 1.19E-02 -2.20E-04 0.54 6.72E+04 13.4

1 1.17E-02 70.4 2.18 0.62 2.7 2.08E-03 1.75E-04 0.43 1.05E-03 141.4

32 7 159.6 2976 10.6 1.44 -3.3 1.20E-02 -1.86E-04 0.54 7.22E+04 15.6

1 1.18E-02 70.4 2.54 0.78 2.76 2.11E-03 1.56E-04 0.46 1.05E-03 140.1

32 8 160.2 3172 12.27 1.76 -4.36 1.22E-02 -2.15E-04 0.55 7.73E+04 17.5

1 1.18E-02 70.4 2.91 0.97 3.71 2.11E-03 1.83E-04 0.49 1.04E-03 139.6

32 9 160.9 3369 14.05 2.14 -4.89 1.23E-02 -2.13E-04 0.55 8.24E+04 19.8

1 1.19E-02 70.4 3.34 1.18 4.4 2.14E-03 1.92E-04 0.52 1.04E-03 138

32 10 161.7 3171 12.42 1.76 -3.72 1.22E-02 -1.82E-04 0.56 7.80E+04 17.9

1 1.19E-02 70.4 2.92 0.98 3.8 2.10E-03 1.86E-04 0.49 1.03E-03 134.4

32 11 162.4 2977 10.81 1.43 -3.16 1.20E-02 -1.75E-04 0.56 7.35E+04 15.7

1 1.20E-02 70.4 2.51 0.8 2.96 2.05E-03 1.64E-04 0.46 1.03E-03 136.9

32 12 163 2779 9.27 1.16 -2.9 1.18E-02 -1.83E-04 0.55 6.89E+04 13.7

1 1.20E-02 70.5 2.18 0.63 2.39 2.03E-03 1.51E-04 0.43 1.03E-03 140.5

32 13 163.6 2583 7.98 0.93 -2.65 1.17E-02 -1.93E-04 0.54 6.43E+04 11.1

1 1.21E-02 70.5 1.89 0.5 2.01 2.03E-03 1.46E-04 0.4 1.02E-03 142.8

32 14 164.4 2386 6.75 0.74 -1.94 1.15E-02 -1.65E-04 0.53 5.96E+04 8

1 1.21E-02 70.5 1.62 0.39 1.45 2.03E-03 1.24E-04 0.37 1.02E-03 143.1

32 15 164.9 2185 5.56 0.57 -1.54 1.13E-02 -1.56E-04 0.51 5.48E+04 3.3

1 1.22E-02 70.5 1.37 0.29 1.45 2.04E-03 1.47E-04 0.34 1.02E-03 136.7

32 16 165.6 1987 4.45 0.44 -1.19 1.09E-02 -1.45E-04 0.47 5.00E+04 NA

1 1.22E-02 70.5 1.16 0.21 0.75 2.08E-03 9.13E-05 0.31 1.01E-03 147.8

32 17 166.2 0 0 0 0 0.00E+00 NA

1 1.23E-02 70.5 0.27 0 0 0 1.01E-03

33 1 166.2 0 0 0 0 0.00E+00 NA

71

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

1 1.23E-02 70.5 0.27 0 0 0 1.01E-03

33 2 167.7 1987 4.59 0.46 -0.67 1.11E-02 -8.05E-05 0.47 5.07E+04 NA

1 1.24E-02 70.6 1.22 0.22 1.13 2.16E-03 1.35E-04 0.31 9.98E-04 120.7

33 3 168.2 2188 5.79 0.6 -1.42 1.15E-02 -1.40E-04 0.51 5.60E+04 4.3

1 1.24E-02 70.6 1.43 0.31 1.67 2.08E-03 1.65E-04 0.34 9.95E-04 130.3

33 4 168.8 2386 6.98 0.76 -2.07 1.16E-02 -1.71E-04 0.53 6.12E+04 8.6

1 1.25E-02 70.6 1.68 0.41 1.91 2.04E-03 1.58E-04 0.37 9.92E-04 137.3

33 5 169.4 2582 8.3 0.97 -2.65 1.18E-02 -1.87E-04 0.54 6.65E+04 11.4

1 1.25E-02 70.6 1.97 0.52 2.24 2.04E-03 1.58E-04 0.4 9.88E-04 139.8

33 6 170 2782 9.73 1.21 -3.01 1.18E-02 -1.82E-04 0.55 7.19E+04 13.7

1 1.26E-02 70.6 2.28 0.66 2.78 2.03E-03 1.68E-04 0.43 9.85E-04 137.3

33 7 170.5 2982 11.3 1.49 -3.54 1.19E-02 -1.86E-04 0.56 7.73E+04 15.6

1 1.26E-02 70.6 2.63 0.83 3.55 2.03E-03 1.86E-04 0.46 9.82E-04 135

33 8 171.1 3173 13.1 1.87 -4.62 1.22E-02 -2.14E-04 0.55 8.25E+04 18

1 1.26E-02 70.6 3.09 1.04 3.78 2.10E-03 1.75E-04 0.49 9.78E-04 140.7

33 9 171.6 3369 14.92 2.25 -4.5 1.23E-02 -1.84E-04 0.56 8.79E+04 19.4

1 1.27E-02 70.6 3.51 1.26 4.48 2.11E-03 1.83E-04 0.52 9.76E-04 135.1

33 10 172.2 3174 13.22 1.84 -4.34 1.22E-02 -1.99E-04 0.57 8.31E+04 17.8

1 1.27E-02 70.6 3.05 1.05 4.05 2.06E-03 1.86E-04 0.49 9.72E-04 137

33 11 172.9 2974 11.52 1.5 -3.83 1.21E-02 -1.99E-04 0.56 7.82E+04 15.7

1 1.28E-02 70.6 2.66 0.85 3.35 2.03E-03 1.74E-04 0.46 9.69E-04 138.8

33 12 173.4 2778 9.96 1.22 -3.35 1.19E-02 -1.99E-04 0.56 7.32E+04 14

1 1.28E-02 70.7 2.3 0.68 2.84 2.01E-03 1.69E-04 0.43 9.66E-04 139.7

33 13 174.1 2581 8.61 0.99 -3.4 1.19E-02 -2.33E-04 0.55 6.83E+04 11.8

1 1.28E-02 70.7 2.01 0.55 2.12 2.03E-03 1.46E-04 0.4 9.62E-04 148

33 14 174.6 2385 7.24 0.78 -2.46 1.17E-02 -1.97E-04 0.54 6.33E+04 8.4

1 1.29E-02 70.7 1.71 0.42 1.86 2.02E-03 1.49E-04 0.37 9.59E-04 142.9

33 15 175.3 2187 6.06 0.61 -1.82 1.16E-02 -1.73E-04 0.53 5.83E+04 3.9

1 1.29E-02 70.7 1.46 0.32 1.41 2.04E-03 1.34E-04 0.34 9.56E-04 142.3

33 16 176 1989 4.87 0.46 -1.5 1.12E-02 -1.72E-04 0.5 5.32E+04 NA

1 1.30E-02 70.7 1.23 0.23 0.91 2.06E-03 1.04E-04 0.31 9.52E-04 148.7

33 17 176.6 0 0 0 0 0.00E+00 NA

1 1.30E-02 70.7 0.27 0 0 0 9.49E-04

72

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

34 1 176.6 0 0 0 0 0.00E+00 NA

1 1.30E-02 70.7 0.27 0 0 0 9.49E-04

34 2 177.9 1989 4.94 0.49 -1.08 1.12E-02 -1.22E-04 0.48 5.38E+04 NA

1 1.31E-02 70.7 1.29 0.24 1.15 2.14E-03 1.30E-04 0.31 9.41E-04 133.2

34 3 178.6 2190 6.27 0.63 -1.85 1.17E-02 -1.72E-04 0.53 5.94E+04 5

1 1.32E-02 70.7 1.51 0.34 1.66 2.06E-03 1.54E-04 0.34 9.38E-04 138.1

34 4 179.2 2383 7.46 0.8 -2.05 1.17E-02 -1.60E-04 0.54 6.49E+04 7.4

1 1.32E-02 70.8 1.77 0.44 2.1 2.03E-03 1.64E-04 0.37 9.35E-04 134.3

34 5 179.8 2583 8.98 1.02 -3.24 1.20E-02 -2.15E-04 0.56 7.06E+04 11.4

1 1.33E-02 70.8 2.07 0.57 2.68 2.03E-03 1.78E-04 0.4 9.31E-04 140.4

34 6 180.4 2778 10.46 1.3 -3.62 1.20E-02 -2.07E-04 0.56 7.62E+04 13.8

1 1.33E-02 70.8 2.45 0.72 3.13 2.06E-03 1.79E-04 0.43 9.29E-04 139.1

34 7 180.9 2977 12.2 1.61 -4.31 1.22E-02 -2.14E-04 0.56 8.18E+04 15.8

1 1.33E-02 70.8 2.85 0.91 3.05 2.08E-03 1.52E-04 0.46 9.26E-04 144.7

34 8 181.4 3177 14 2 -4.74 1.23E-02 -2.06E-04 0.56 8.76E+04 18

1 1.34E-02 70.8 3.3 1.11 4.25 2.11E-03 1.85E-04 0.49 9.23E-04 138.1

34 9 181.9 3370 15.99 2.4 -5.17 1.24E-02 -1.99E-04 0.56 9.32E+04 19.6

1 1.34E-02 70.8 3.75 1.35 4.7 2.12E-03 1.81E-04 0.52 9.21E-04 137.7

34 10 182.5 3172 14.18 1.98 -4.84 1.24E-02 -2.10E-04 0.57 8.80E+04 18.1

1 1.35E-02 70.8 3.28 1.13 4.11 2.09E-03 1.78E-04 0.49 9.18E-04 139.7

34 11 183.1 2976 12.32 1.61 -3.34 1.22E-02 -1.64E-04 0.57 8.28E+04 15.8

1 1.35E-02 70.8 2.83 0.91 3.32 2.05E-03 1.63E-04 0.46 9.15E-04 135.1

34 12 183.7 2781 10.65 1.33 -3.17 1.20E-02 -1.77E-04 0.55 7.76E+04 13.7

1 1.36E-02 70.8 2.5 0.73 3 2.07E-03 1.68E-04 0.43 9.12E-04 136.5

34 13 184.4 2580 9.12 1.03 -2.4 1.19E-02 -1.56E-04 0.56 7.23E+04 11.6

1 1.36E-02 70.8 2.11 0.58 2.54 2.01E-03 1.65E-04 0.4 9.09E-04 133.3

34 14 184.8 2383 7.75 0.82 -2.3 1.18E-02 -1.74E-04 0.55 6.69E+04 8.7

1 1.36E-02 70.9 1.81 0.45 1.77 2.02E-03 1.34E-04 0.37 9.06E-04 142.4

34 15 185.6 2187 6.45 0.64 -1.91 1.17E-02 -1.71E-04 0.54 6.17E+04 4.4

1 1.37E-02 70.9 1.54 0.34 1.6 2.03E-03 1.43E-04 0.34 9.03E-04 140.1

34 16 186.1 1991 5.18 0.49 -1.4 1.12E-02 -1.51E-04 0.5 5.63E+04 NA

1 1.37E-02 70.9 1.3 0.25 1.03 2.06E-03 1.12E-04 0.31 9.00E-04 143.6

73

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

34 17 186.7 0 0 0 0 0.00E+00 NA

1 1.38E-02 70.9 0.28 0 0 0 8.98E-04

35 1 186.7 0 0 0 0 0.00E+00 NA

1 1.38E-02 70.9 0.28 0 0 0 8.98E-04

35 2 187.8 1994 5.32 0.5 -1.27 1.14E-02 -1.35E-04 0.51 5.69E+04 NA

1 1.39E-02 70.9 1.33 0.26 1.22 2.09E-03 1.30E-04 0.31 8.92E-04 136.1

35 3 188.4 2192 6.63 0.67 -2.08 1.17E-02 -1.83E-04 0.53 6.27E+04 4.8

1 1.39E-02 70.9 1.6 0.36 1.83 2.07E-03 1.61E-04 0.34 8.89E-04 138.6

35 4 188.9 2384 7.97 0.85 -2.45 1.19E-02 -1.82E-04 0.55 6.84E+04 8.1

1 1.39E-02 70.9 1.86 0.47 1.82 2.03E-03 1.35E-04 0.37 8.87E-04 143.3

35 5 189.4 2581 9.52 1.08 -3.59 1.21E-02 -2.26E-04 0.57 7.43E+04 11.3

1 1.40E-02 70.9 2.19 0.61 2.65 2.03E-03 1.67E-04 0.4 8.85E-04 143.5

35 6 190 2778 11.15 1.35 -4.1 1.22E-02 -2.22E-04 0.57 8.02E+04 13.5

1 1.40E-02 70.9 2.55 0.77 3.06 2.04E-03 1.66E-04 0.43 8.82E-04 143.2

35 7 190.5 2975 12.88 1.69 -4.35 1.22E-02 -2.05E-04 0.57 8.61E+04 16.1

1 1.41E-02 70.9 2.98 0.96 3.5 2.07E-03 1.66E-04 0.46 8.80E-04 141.1

35 8 191.1 3173 14.86 2.06 -5.25 1.24E-02 -2.17E-04 0.58 9.21E+04 17.7

1 1.41E-02 71 3.41 1.18 4.53 2.08E-03 1.88E-04 0.49 8.77E-04 139.2

35 9 191.6 3368 16.96 2.54 -6.06 1.25E-02 -2.22E-04 0.57 9.80E+04 20

1 1.41E-02 71 3.96 1.44 5.61 2.13E-03 2.05E-04 0.52 8.75E-04 137.2

35 10 192.1 3171 14.99 2.05 -5.1 1.24E-02 -2.10E-04 0.59 9.25E+04 18

1 1.42E-02 71 3.39 1.2 4.78 2.05E-03 1.97E-04 0.49 8.72E-04 136.8

35 11 192.8 2975 13.19 1.69 -4.67 1.24E-02 -2.18E-04 0.58 8.71E+04 15.8

1 1.42E-02 71 2.99 0.99 3.78 2.05E-03 1.77E-04 0.46 8.69E-04 141

35 12 193.4 2780 11.41 1.36 -3.91 1.22E-02 -2.08E-04 0.58 8.17E+04 14.1

1 1.43E-02 71 2.57 0.79 3.49 2.01E-03 1.86E-04 0.43 8.66E-04 138.3

35 13 193.9 2581 9.81 1.09 -3.79 1.22E-02 -2.34E-04 0.58 7.60E+04 11.4

1 1.43E-02 71 2.22 0.63 2.77 2.01E-03 1.71E-04 0.4 8.64E-04 143.9

35 14 194.6 2384 8.34 0.86 -3.55 1.21E-02 -2.55E-04 0.57 7.05E+04 9.4

1 1.44E-02 71 1.9 0.49 2.37 2.02E-03 1.71E-04 0.37 8.61E-04 146.2

35 15 195.3 2185 6.94 0.68 -2.63 1.19E-02 -2.25E-04 0.55 6.48E+04 4.6

1 1.44E-02 71.1 1.64 0.37 1.94 2.06E-03 1.66E-04 0.34 8.58E-04 143.6

74

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

35 16 195.9 1989 5.6 0.52 -1.98 1.16E-02 -2.04E-04 0.52 5.92E+04 NA

1 1.45E-02 71.1 1.37 0.27 1.46 2.07E-03 1.50E-04 0.31 8.55E-04 143.7

35 17 196.5 987 1.02 0.08 -0.15 8.58E-03 -6.21E-05 0.27 2.95E+04 NA

1 1.45E-02 71.1 0.42 0.02 0.08 2.60E-03 3.33E-05 0.15 8.53E-04 151.8

35 18 197.2 0 0 0 0 0.00E+00 NA

1 1.45E-02 71.1 0.28 0 0 0 8.50E-04

36 1 1014.7 0 0 0 0 0.00E+00 NA

1 7.32E-02 83.1 0.38 0 0 0 1.71E-04

36 2 1014.7 500 1.91 0.05 -0.9 1.23E-02 -2.89E-04 0.45 7.45E+04 3.2

1 7.32E-02 82.7 0.55 0.02 0.08 2.60E-03 2.44E-05 0.08 1.71E-04 175.2

36 3 1014.7 1202 11.21 0.55 -4.74 1.25E-02 -2.63E-04 0.62 1.79E+05 8.6

1 7.33E-02 82.4 2.4 0.34 2.85 1.96E-03 1.58E-04 0.18 1.71E-04 149

36 4 1014.7 1593 20.11 1.23 -7.2 1.28E-02 -2.27E-04 0.67 2.38E+05 11.9

1 7.33E-02 82.1 4.04 0.82 6.73 1.88E-03 2.13E-04 0.25 1.71E-04 136.9

36 5 1014.7 2085 35.51 2.73 -13.98 1.32E-02 -2.58E-04 0.7 3.12E+05 15.7

1 7.34E-02 81.8 6.88 1.92 12.61 1.86E-03 2.32E-04 0.32 1.70E-04 137.9

36 6 1014.7 0 0 0 0 0.00E+00 NA

1 7.34E-02 81.5 0.43 0 0 0 1.70E-04

37 1 1016.5 0 0 0 0 0.00E+00 NA

2 7.53E-02 68.8 0.28 0 0 0 1.63E-04

37 2 1016.6 500 3.36 0.07 -0.51 2.11E-02 -1.58E-04 0.75 7.82E+04 4

2 7.53E-02 68.8 0.77 0.06 2.04 3.53E-03 6.38E-04 0.08 1.63E-04 103.9

37 3 1016.6 998 14.15 0.59 -5.12 2.23E-02 -4.01E-04 0.8 1.56E+05 9.3

2 7.53E-02 68.8 3.13 0.48 8.15 3.60E-03 6.38E-04 0.16 1.63E-04 122.1

37 4 1016.6 1244 21.81 1.14 -7.33 2.21E-02 -3.70E-04 0.8 1.95E+05 11.4

2 7.53E-02 68.8 4.83 0.91 11.98 3.58E-03 6.04E-04 0.19 1.63E-04 121.5

37 5 1016.5 997 13.87 0.58 -5.41 2.19E-02 -4.25E-04 0.79 1.56E+05 9

2 7.53E-02 68.8 3.08 0.46 7.61 3.56E-03 5.97E-04 0.16 1.63E-04 125.4

37 6 1016.6 500 3.26 0.07 -1.1 2.05E-02 -3.42E-04 0.74 7.82E+04 4.3

2 7.53E-02 68.8 0.75 0.05 1.54 3.43E-03 4.82E-04 0.08 1.63E-04 125.4

37 7 1016.6 0 0 0 0 0.00E+00 NA 75

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 7.53E-02 68.8 0.31 0 0 0 1.63E-04

38 1 9.7 0 0 0 0 0.00E+00 NA

2 7.41E-04 53.1 0.24 0 0 0 1.71E-02

38 2 10.9 2182 0.24 0.08 0.07 7.27E-03 1.07E-04 0.12 3.64E+03 NA

2 8.29E-04 53.4 0.2 0.01 0.41 4.37E-03 6.04E-04 0.34 1.52E-02 79.9

38 3 11.7 2579 0.48 0.13 0.29 9.52E-03 2.90E-04 0.2 4.62E+03 NA

2 8.89E-04 53.7 0.27 0.03 0.21 3.94E-03 2.08E-04 0.41 1.42E-02 35.7

38 4 12.4 2975 0.74 0.21 0.32 1.05E-02 2.29E-04 0.25 5.66E+03 NA

2 9.42E-04 53.9 0.37 0.05 0.66 3.80E-03 4.64E-04 0.47 1.34E-02 63.8

38 5 13.1 3365 1.18 0.53 0.71 1.23E-02 3.69E-04 0.19 6.81E+03 NA

2 1.00E-03 54.2 0.83 0.1 0.3 6.30E-03 1.54E-04 0.53 1.26E-02 22.7

38 6 14.1 2973 1.24 0.37 0.62 1.54E-02 3.83E-04 0.28 6.46E+03 NA

2 1.07E-03 54.4 0.65 0.1 -0.41 5.90E-03 -2.53E-04 0.47 1.17E-02 -33.4

38 7 15.1 2577 0.99 0.24 0.93 1.54E-02 7.20E-04 0.3 6.00E+03 NA

2 1.15E-03 54.6 0.49 0.07 -0.72 5.54E-03 -5.56E-04 0.41 1.09E-02 -37.7

38 8 16 2184 0.68 0.12 1.32 1.38E-02 1.34E-03 0.34 5.41E+03 NA

2 1.22E-03 54.9 0.28 0.04 0.2 4.12E-03 2.00E-04 0.34 1.03E-02 8.5

38 9 16.8 0 0 0 0 0.00E+00 NA

2 1.27E-03 55.1 0.25 0 0 0 9.82E-03

39 1 16.8 0 0 0 0 0.00E+00 NA

2 1.27E-03 55.1 0.25 0 0 0 9.82E-03

39 2 17.8 2184 0.59 0.13 0.81 1.09E-02 7.40E-04 0.24 6.01E+03 NA

2 1.35E-03 55.4 0.31 0.03 0.17 4.11E-03 1.56E-04 0.34 9.25E-03 11.9

39 3 18.5 2579 0.99 0.2 0.4 1.24E-02 2.49E-04 0.31 7.40E+03 NA

2 1.41E-03 55.6 0.42 0.06 0.13 3.84E-03 7.90E-05 0.41 8.88E-03 17.6

39 4 19.2 2974 1.47 0.33 -0.03 1.35E-02 -1.37E-05 0.35 8.82E+03 NA

2 1.45E-03 55.8 0.58 0.12 0.55 3.92E-03 2.50E-04 0.47 8.59E-03 93.1

39 5 19.9 3374 2.04 0.65 0.24 1.40E-02 8.31E-05 0.28 1.04E+04 NA

2 1.51E-03 56 1.02 0.18 0.55 5.10E-03 1.88E-04 0.53 8.26E-03 66.1

39 6 20.7 2974 1.89 0.45 0.47 1.61E-02 2.01E-04 0.35 9.51E+03 NA

2 1.57E-03 56.2 0.8 0.16 0.37 5.00E-03 1.57E-04 0.47 7.96E-03 38.1

76

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

39 7 21.4 2578 1.48 0.27 0.73 1.62E-02 3.98E-04 0.4 8.52E+03 NA

2 1.62E-03 56.4 0.56 0.11 -0.06 4.47E-03 -3.06E-05 0.41 7.70E-03 -4.4

39 8 22.4 2184 1.02 0.15 0.82 1.49E-02 5.98E-04 0.41 7.56E+03 NA

2 1.70E-03 56.7 0.36 0.06 0.47 3.89E-03 3.43E-04 0.34 7.35E-03 29.8

39 9 23 0 0.14 0 -0.62 0.00E+00 NA

2 1.74E-03 56.8 0.26 0 0 0 7.16E-03 179.9

40 1 30.7 0 0 0 0 0.00E+00 NA

2 2.32E-03 58.6 0.26 0 0 0 5.37E-03

40 2 31.6 2190 1.37 0.22 1.22 1.41E-02 6.27E-04 0.37 1.07E+04 NA

2 2.39E-03 58.8 0.53 0.08 0.38 3.98E-03 1.93E-04 0.34 5.21E-03 17.1

40 3 32.2 2583 2.06 0.35 1.01 1.50E-02 3.67E-04 0.42 1.29E+04 NA

2 2.43E-03 58.9 0.71 0.15 0.36 3.77E-03 1.31E-04 0.41 5.11E-03 19.7

40 4 32.9 2974 2.88 0.56 0.98 1.55E-02 2.61E-04 0.43 1.51E+04 NA

2 2.48E-03 59 0.98 0.24 0.96 3.86E-03 2.57E-04 0.47 5.01E-03 44.6

40 5 33.6 3368 3.79 0.97 0.98 1.56E-02 2.00E-04 0.37 1.75E+04 NA

2 2.53E-03 59.1 1.51 0.36 1.26 4.53E-03 2.58E-04 0.53 4.91E-03 52.3

40 6 34.2 2975 3.17 0.66 0.88 1.64E-02 2.26E-04 0.41 1.57E+04 NA

2 2.58E-03 59.2 1.17 0.27 1.17 4.43E-03 3.01E-04 0.47 4.82E-03 53.1

40 7 34.8 2579 2.35 0.38 1.52 1.59E-02 5.12E-04 0.46 1.39E+04 NA

2 2.62E-03 59.3 0.77 0.17 0.18 3.79E-03 6.17E-05 0.41 4.74E-03 6.9

40 8 35.4 2193 1.62 0.24 1.49 1.49E-02 6.80E-04 0.41 1.20E+04 NA

2 2.67E-03 59.4 0.57 0.1 0.54 3.81E-03 2.46E-04 0.34 4.65E-03 19.9

40 9 36.1 0 0 0 0 0.00E+00 NA

2 2.72E-03 59.4 0.24 0 0 0 4.56E-03

41 1 36.1 0 0 0 0 0.00E+00 NA

2 2.72E-03 59.4 0.24 0 0 0 4.56E-03

41 2 37.1 2190 1.59 0.25 0.94 1.40E-02 4.14E-04 0.37 1.26E+04 NA

2 2.80E-03 59.6 0.6 0.09 0.8 3.84E-03 3.52E-04 0.34 4.44E-03 40.4

41 3 37.7 2578 2.45 0.4 0.83 1.53E-02 2.58E-04 0.44 1.50E+04 NA

2 2.84E-03 59.7 0.82 0.18 0.81 3.77E-03 2.53E-04 0.41 4.37E-03 44.4

41 4 38.4 2975 3.42 0.63 0.59 1.58E-02 1.36E-04 0.45 1.76E+04 NA 77

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 2.89E-03 59.8 1.12 0.29 1.78 3.78E-03 4.09E-04 0.47 4.29E-03 71.6

41 5 39.1 3367 4.46 0.96 0.43 1.58E-02 7.58E-05 0.44 2.03E+04 NA

2 2.94E-03 59.9 1.5 0.43 1.8 3.89E-03 3.16E-04 0.53 4.21E-03 76.5

41 6 39.7 2976 3.62 0.66 0.67 1.62E-02 1.48E-04 0.47 1.83E+04 NA

2 2.99E-03 60 1.17 0.31 1.7 3.82E-03 3.78E-04 0.47 4.15E-03 68.6

41 7 40.5 2576 2.64 0.43 1.14 1.55E-02 3.32E-04 0.44 1.61E+04 NA

2 3.05E-03 60 0.88 0.19 0.91 3.77E-03 2.64E-04 0.4 4.07E-03 38.5

41 8 41.2 2182 1.77 0.27 1.28 1.42E-02 5.08E-04 0.39 1.39E+04 NA

2 3.10E-03 60.1 0.65 0.1 0.81 3.78E-03 3.24E-04 0.34 4.00E-03 32.5

41 9 42 0 0 0 0 0.00E+00 NA

2 3.16E-03 60.2 0.26 0 0 0 3.92E-03

42 1 42 0 0 0 0 0.00E+00 NA

2 3.16E-03 60.2 0.26 0 0 0 3.92E-03

42 2 42.9 2185 1.88 0.28 0.7 1.44E-02 2.68E-04 0.39 1.45E+04 NA

2 3.23E-03 60.3 0.68 0.11 0.83 3.84E-03 3.15E-04 0.34 3.84E-03 49.6

42 3 43.6 2581 2.96 0.47 0.45 1.60E-02 1.21E-04 0.47 1.74E+04 NA

2 3.29E-03 60.5 0.95 0.22 0.91 3.75E-03 2.45E-04 0.41 3.78E-03 63.6

42 4 45 2581 3.05 0.48 0.33 1.60E-02 8.48E-05 0.47 1.80E+04 NA

2 3.39E-03 60.7 0.98 0.22 1.23 3.75E-03 3.21E-04 0.41 3.66E-03 75.2

42 5 45.9 2979 4.32 0.76 -0.25 1.67E-02 -4.73E-05 0.49 2.11E+04 NA

2 3.45E-03 60.8 1.34 0.37 2.11 3.79E-03 4.06E-04 0.47 3.59E-03 96.7

42 6 46.6 3374 5.66 1.3 0.1 1.68E-02 1.48E-05 0.43 2.43E+04 NA

2 3.51E-03 60.9 2.02 0.56 2.67 4.37E-03 3.93E-04 0.53 3.54E-03 87.8

42 7 47.4 2973 4.56 0.79 0.99 1.71E-02 1.84E-04 0.51 2.18E+04 NA

2 3.56E-03 60.9 1.4 0.4 2.43 3.83E-03 4.52E-04 0.47 3.48E-03 67.8

42 8 48.1 2584 3.2 0.52 1.29 1.57E-02 3.15E-04 0.45 1.92E+04 NA

2 3.61E-03 61 1.05 0.23 0.99 3.75E-03 2.42E-04 0.41 3.43E-03 37.5

42 9 48.8 2184 2.28 0.32 1.09 1.54E-02 3.65E-04 0.44 1.65E+04 NA

2 3.67E-03 61.1 0.77 0.14 1.22 3.78E-03 4.09E-04 0.34 3.38E-03 48.2

42 10 49.5 0 0 0 0 0.00E+00 NA

2 3.72E-03 61.1 0.24 0 0 0 3.33E-03

78

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

43 1 49.5 0 0 0 0 0.00E+00 NA

2 3.72E-03 61.1 0.24 0 0 0 3.33E-03

43 2 50.3 2186 2.26 0.33 0.41 1.48E-02 1.34E-04 0.41 1.70E+04 NA

2 3.78E-03 61.2 0.8 0.14 1.1 3.84E-03 3.57E-04 0.34 3.28E-03 69.5

43 3 51.1 2578 3.4 0.54 0.18 1.57E-02 4.17E-05 0.46 2.03E+04 NA

2 3.84E-03 61.3 1.11 0.25 1.14 3.74E-03 2.62E-04 0.4 3.23E-03 80.9

43 4 52 2980 4.96 0.86 -0.36 1.69E-02 -6.02E-05 0.5 2.39E+04 NA

2 3.91E-03 61.4 1.52 0.43 2.71 3.79E-03 4.59E-04 0.47 3.17E-03 97.5

43 5 52.7 3375 6.51 1.32 -0.29 1.71E-02 -3.77E-05 0.49 2.74E+04 NA

2 3.96E-03 61.5 2.05 0.65 3.37 3.94E-03 4.40E-04 0.53 3.13E-03 94.9

43 6 53.3 2974 5.2 0.89 0.15 1.74E-02 2.42E-05 0.52 2.45E+04 NA

2 4.00E-03 61.6 1.57 0.46 2.49 3.83E-03 4.12E-04 0.47 3.09E-03 86.6

43 7 54.1 2574 3.8 0.57 0.59 1.67E-02 1.28E-04 0.5 2.15E+04 NA

2 4.06E-03 61.6 1.17 0.28 1.53 3.76E-03 3.33E-04 0.4 3.05E-03 68.9

43 8 54.8 2185 2.67 0.36 0.78 1.61E-02 2.34E-04 0.47 1.85E+04 NA

2 4.11E-03 61.7 0.86 0.17 1.65 3.78E-03 4.94E-04 0.34 3.01E-03 64.6

43 9 51 0 0 0 0 0.00E+00 NA

2 3.83E-03 61.8 0.24 0 0 0 3.24E-03

44 1 51 0 0 0 0 0.00E+00 NA

2 3.83E-03 61.8 0.24 0 0 0 3.24E-03

44 2 40.5 2193 1.85 0.28 0.53 1.50E-02 2.15E-04 0.4 1.36E+04 NA

2 3.04E-03 61.7 0.68 0.11 0.87 4.01E-03 3.49E-04 0.34 4.10E-03 58.4

44 3 30.4 2586 1.9 0.34 0.35 1.47E-02 1.34E-04 0.39 1.21E+04 NA

2 2.29E-03 61.4 0.69 0.13 0.48 3.91E-03 1.85E-04 0.41 5.45E-03 54.1

44 4 24.8 2981 2.21 0.43 -0.12 1.58E-02 -4.36E-05 0.43 1.14E+04 NA

2 1.87E-03 61.1 0.76 0.19 1.21 3.98E-03 4.30E-04 0.47 6.67E-03 95.8

44 5 20 3371 2.24 0.52 0.01 1.55E-02 2.98E-06 0.4 1.04E+04 NA

2 1.50E-03 60.7 0.82 0.21 1.19 4.12E-03 4.11E-04 0.53 8.29E-03 89.6

44 6 16.2 2974 1.38 0.28 -0.03 1.51E-02 -1.49E-05 0.4 7.39E+03 NA

2 1.22E-03 60.5 0.5 0.11 0.83 4.00E-03 4.55E-04 0.47 1.02E-02 91.9

44 7 12.4 2581 0.7 0.14 0.75 1.33E-02 7.05E-04 0.33 4.90E+03 NA

2 9.36E-04 60.4 0.29 0.05 -0.17 4.03E-03 -1.57E-04 0.41 1.34E-02 -12.6 79

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

44 8 10.3 2184 0.44 0.08 0.8 1.40E-02 1.27E-03 0.32 3.43E+03 NA

2 7.78E-04 60.5 0.19 0.03 0.37 4.52E-03 5.86E-04 0.34 1.62E-02 24.9

44 9 8.6 0 0 0 0 0.00E+00 NA

2 6.49E-04 60.5 0.24 0 0 0 1.95E-02

45 1 8.6 0 0 0 0 0.00E+00 NA

2 6.49E-04 60.5 0.24 0 0 0 1.95E-02

45 2 7 2184 0.22 0.06 0.3 1.05E-02 6.94E-04 0.18 2.30E+03 NA

2 5.27E-04 60.5 0.15 0.01 -0.14 5.11E-03 -3.39E-04 0.34 2.42E-02 -26

45 3 6 2577 0.25 0.08 0.43 9.76E-03 8.49E-04 0.19 2.32E+03 NA

2 4.52E-04 60.5 0.15 0.01 -0.55 4.41E-03 -1.07E-03 0.4 2.83E-02 -51.6

45 4 5.8 2980 0.67 0.11 1.07 2.03E-02 1.62E-03 0.6 2.58E+03 NA

2 4.37E-04 60.6 0.19 0.06 0.25 4.20E-03 3.84E-04 0.47 2.94E-02 13.4

45 5 6.6 2577 0.41 0.08 1.48 1.47E-02 2.64E-03 0.38 2.53E+03 NA

2 4.96E-04 60.6 0.15 0.03 -0.39 4.03E-03 -7.03E-04 0.4 2.59E-02 -14.9

45 6 7.4 2183 0.31 0.06 1.22 1.38E-02 2.69E-03 0.31 2.42E+03 NA

2 5.59E-04 60.7 0.14 0.02 0.18 4.49E-03 3.95E-04 0.34 2.30E-02 8.4

45 7 8.3 0 0 0 0 0.00E+00 NA

2 6.26E-04 60.7 0.24 0 0 0 2.05E-02

46 1 8.3 0 0 0 0 0.00E+00 NA

2 6.26E-04 60.7 0.24 0 0 0 2.05E-02

46 2 9.2 2186 0.27 0.07 0.29 9.79E-03 5.23E-04 0.19 3.00E+03 NA

2 6.90E-04 60.8 0.17 0.01 -0.04 4.37E-03 -7.42E-05 0.34 1.85E-02 -8.1

46 3 9.8 2575 0.41 0.11 0.46 9.92E-03 5.47E-04 0.23 3.80E+03 NA

2 7.39E-04 60.9 0.21 0.02 -0.26 3.78E-03 -3.14E-04 0.4 1.73E-02 -29.9

46 4 10.5 2975 0.8 0.17 0.03 1.35E-02 2.27E-05 0.36 4.67E+03 NA

2 7.87E-04 60.9 0.3 0.06 0.16 3.77E-03 1.34E-04 0.47 1.62E-02 80.4

46 5 11.1 3373 1.06 0.29 0.2 1.31E-02 1.22E-04 0.31 5.64E+03 NA

2 8.36E-04 61 0.46 0.09 0.24 4.16E-03 1.48E-04 0.53 1.52E-02 50.5

46 6 11.9 2981 0.95 0.2 0.25 1.42E-02 1.83E-04 0.39 5.34E+03 NA

2 8.93E-04 61.1 0.35 0.08 0.37 3.81E-03 2.74E-04 0.47 1.42E-02 56.3

46 7 12.7 2577 0.66 0.14 0.88 1.23E-02 8.15E-04 0.32 4.94E+03 NA

80

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 9.54E-04 61.2 0.28 0.04 -0.12 3.75E-03 -1.10E-04 0.4 1.33E-02 -7.7

46 8 13.4 2183 0.49 0.09 0.77 1.21E-02 9.41E-04 0.29 4.44E+03 NA

2 1.01E-03 61.3 0.22 0.03 0.15 3.97E-03 1.87E-04 0.34 1.25E-02 11.2

46 9 14.2 0 0 0 0 0.00E+00 NA

2 1.07E-03 61.4 0.23 0 0 0 1.19E-02

47 1 14.2 0 0 0 0 0.00E+00 NA

2 1.07E-03 61.4 0.23 0 0 0 1.19E-02

47 2 15.2 2183 0.52 0.11 0.41 1.12E-02 4.47E-04 0.26 5.03E+03 NA

2 1.14E-03 61.6 0.25 0.03 0.06 4.02E-03 6.17E-05 0.34 1.11E-02 7.9

47 3 15.9 2579 0.78 0.17 0.57 1.16E-02 4.25E-04 0.29 6.21E+03 NA

2 1.19E-03 61.7 0.34 0.05 -0.12 3.72E-03 -8.67E-05 0.4 1.06E-02 -11.5

47 4 16.7 2974 1.24 0.27 0.23 1.33E-02 1.23E-04 0.36 7.52E+03 NA

2 1.25E-03 61.8 0.47 0.1 0.36 3.71E-03 1.92E-04 0.47 1.01E-02 57.4

47 5 17.4 3375 1.74 0.46 0.6 1.38E-02 2.35E-04 0.34 8.93E+03 NA

2 1.31E-03 61.9 0.71 0.16 0.62 4.11E-03 2.46E-04 0.53 9.62E-03 46.3

47 6 18 2979 1.47 0.29 0.65 1.44E-02 3.17E-04 0.41 8.17E+03 NA

2 1.35E-03 62 0.52 0.12 0.64 3.71E-03 3.12E-04 0.47 9.29E-03 44.6

47 7 18.7 2581 0.99 0.19 1.2 1.25E-02 7.52E-04 0.33 7.35E+03 NA

2 1.41E-03 62.1 0.4 0.06 0.02 3.66E-03 1.21E-05 0.4 8.94E-03 0.9

47 8 19.9 2181 0.76 0.13 0.95 1.27E-02 7.89E-04 0.33 6.59E+03 NA

2 1.49E-03 62.3 0.31 0.04 0.3 3.81E-03 2.50E-04 0.34 8.42E-03 17.6

47 9 20.6 0 0 0 0 0.00E+00 NA

2 1.55E-03 62.4 0.25 0 0 0 8.11E-03

48 1 20.6 0 0 0 0 0.00E+00 NA

2 1.55E-03 62.4 0.25 0 0 0 8.11E-03

48 2 21.4 2188 0.82 0.14 0.55 1.25E-02 4.18E-04 0.32 7.12E+03 NA

2 1.61E-03 62.5 0.34 0.05 0.05 3.84E-03 3.79E-05 0.34 7.82E-03 5.2

48 3 22.2 2580 1.18 0.23 0.45 1.26E-02 2.41E-04 0.34 8.70E+03 NA

2 1.66E-03 62.7 0.47 0.08 0.02 3.65E-03 1.13E-05 0.4 7.55E-03 2.7

48 4 22.8 2974 1.79 0.37 0.13 1.40E-02 4.87E-05 0.39 1.03E+04 NA

2 1.71E-03 62.7 0.65 0.14 0.54 3.72E-03 2.11E-04 0.47 7.34E-03 77 81

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

48 5 23.5 3371 2.36 0.57 0.55 1.40E-02 1.60E-04 0.37 1.21E+04 NA

2 1.76E-03 62.8 0.89 0.21 0.67 3.86E-03 1.97E-04 0.53 7.11E-03 50.8

48 6 24.2 2975 2.02 0.4 0.36 1.49E-02 1.31E-04 0.41 1.10E+04 NA

2 1.81E-03 62.9 0.7 0.17 0.88 3.79E-03 3.22E-04 0.47 6.91E-03 67.9

48 7 24.7 2582 1.44 0.26 0.81 1.38E-02 3.87E-04 0.38 9.73E+03 NA

2 1.85E-03 62.9 0.53 0.1 0.22 3.68E-03 1.07E-04 0.4 6.75E-03 15.4

48 8 25.5 2183 1.09 0.17 0.7 1.42E-02 4.53E-04 0.39 8.47E+03 NA

2 1.91E-03 63 0.4 0.06 0.32 3.79E-03 2.09E-04 0.34 6.56E-03 24.7

48 9 26 0 0 0 0 0.00E+00 NA

2 1.95E-03 63.1 0.25 0 0 0 6.42E-03

49 1 26 0 0 0 0 0.00E+00 NA

2 1.95E-03 63.1 0.25 0 0 0 6.42E-03

49 2 27 2186 1.07 0.18 0.54 1.31E-02 3.26E-04 0.34 8.98E+03 NA

2 2.02E-03 63.2 0.43 0.06 0.19 3.82E-03 1.17E-04 0.34 6.20E-03 19.7

49 3 27.7 2584 1.58 0.29 0.58 1.35E-02 2.47E-04 0.37 1.09E+04 NA

2 2.08E-03 63.3 0.59 0.11 0.24 3.67E-03 1.03E-04 0.4 6.02E-03 22.6

49 4 28.5 2973 2.36 0.46 0.14 1.48E-02 4.43E-05 0.42 1.29E+04 NA

2 2.13E-03 63.4 0.81 0.19 0.96 3.72E-03 2.98E-04 0.47 5.85E-03 81.5

49 5 29.2 3371 3.09 0.76 0.29 1.47E-02 6.75E-05 0.38 1.50E+04 NA

2 2.19E-03 63.5 1.18 0.28 1.24 4.10E-03 2.93E-04 0.53 5.71E-03 77

49 6 29.9 2975 2.52 0.48 0.44 1.50E-02 1.30E-04 0.43 1.36E+04 NA

2 2.24E-03 63.6 0.85 0.21 1.06 3.73E-03 3.13E-04 0.47 5.58E-03 67.5

49 7 30.6 2577 1.75 0.32 0.77 1.36E-02 2.97E-04 0.38 1.20E+04 NA

2 2.29E-03 63.6 0.65 0.12 0.39 3.68E-03 1.53E-04 0.4 5.46E-03 27.2

49 8 31.3 2186 1.3 0.2 0.68 1.38E-02 3.58E-04 0.37 1.04E+04 NA

2 2.34E-03 63.6 0.49 0.08 0.42 3.77E-03 2.23E-04 0.34 5.34E-03 31.9

49 9 31.9 0 0 0 0 0.00E+00 NA

2 2.39E-03 63.7 0.25 0 0 0 5.23E-03

50 1 31.9 0 0 0 0 0.00E+00 NA

2 2.39E-03 63.7 0.25 0 0 0 5.23E-03

50 2 32.9 2183 1.35 0.21 0.25 1.36E-02 1.24E-04 0.36 1.10E+04 NA

82

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 2.46E-03 63.8 0.52 0.08 0.16 3.81E-03 7.80E-05 0.34 5.06E-03 32.1

50 3 33.6 2578 1.97 0.35 0.43 1.39E-02 1.53E-04 0.39 1.32E+04 NA

2 2.51E-03 63.9 0.71 0.14 0.5 3.69E-03 1.76E-04 0.4 4.96E-03 49

50 4 34.3 2976 2.92 0.55 -0.07 1.52E-02 -1.75E-05 0.44 1.56E+04 NA

2 2.56E-03 63.9 0.98 0.24 1.14 3.72E-03 2.94E-04 0.47 4.86E-03 93.4

50 5 34.8 3365 3.82 0.86 0.14 1.53E-02 2.71E-05 0.42 1.79E+04 NA

2 2.60E-03 64 1.34 0.36 1.69 3.92E-03 3.37E-04 0.53 4.79E-03 85.4

50 6 35.5 2975 3.11 0.58 0.21 1.57E-02 5.38E-05 0.45 1.61E+04 NA

2 2.65E-03 64 1.03 0.26 1.44 3.78E-03 3.61E-04 0.47 4.70E-03 81.5

50 7 36 2581 2.24 0.38 0.53 1.47E-02 1.74E-04 0.42 1.42E+04 NA

2 2.69E-03 64.1 0.77 0.16 0.83 3.73E-03 2.72E-04 0.4 4.63E-03 57.5

50 8 37.2 2183 1.67 0.24 0.42 1.49E-02 1.87E-04 0.42 1.24E+04 NA

2 2.78E-03 64.2 0.58 0.1 0.85 3.81E-03 3.76E-04 0.34 4.48E-03 63.6

50 9 38.2 2182 1.66 0.25 0.54 1.44E-02 2.34E-04 0.4 1.27E+04 NA

2 2.85E-03 64.3 0.6 0.1 0.78 3.80E-03 3.38E-04 0.34 4.36E-03 55.3

50 10 38.9 0 0 0 0 0.00E+00 NA

2 2.91E-03 64.3 0.23 0 0 0 4.28E-03

51 1 40.2 0 0 0 0 0.00E+00 NA

2 3.00E-03 64.5 0.24 0 0 0 4.15E-03

51 2 41.4 2188 1.87 0.27 0.34 1.49E-02 1.35E-04 0.41 1.38E+04 NA

2 3.09E-03 64.6 0.66 0.11 0.89 3.84E-03 3.54E-04 0.34 4.03E-03 69.1

51 3 42.1 2579 2.61 0.45 0.42 1.48E-02 1.18E-04 0.41 1.66E+04 NA

2 3.14E-03 64.7 0.93 0.19 1.05 3.83E-03 2.96E-04 0.4 3.96E-03 68.3

51 4 42.8 2976 3.63 0.71 0.29 1.52E-02 6.04E-05 0.42 1.94E+04 NA

2 3.19E-03 64.7 1.26 0.3 1.38 3.85E-03 2.86E-04 0.47 3.90E-03 78.1

51 5 43.3 3368 4.75 1.06 0.42 1.53E-02 6.69E-05 0.42 2.23E+04 NA

2 3.23E-03 64.8 1.66 0.45 2.06 3.91E-03 3.30E-04 0.53 3.85E-03 78.5

51 6 44 2975 3.87 0.73 0.04 1.58E-02 7.99E-06 0.45 2.00E+04 NA

2 3.28E-03 64.8 1.29 0.33 1.78 3.83E-03 3.61E-04 0.47 3.79E-03 88.7

51 7 44.5 2581 2.76 0.47 0.58 1.48E-02 1.55E-04 0.42 1.75E+04 NA

2 3.32E-03 64.8 0.96 0.2 1.19 3.74E-03 3.16E-04 0.4 3.75E-03 63.9

51 8 45.1 2185 2.05 0.29 0.48 1.51E-02 1.77E-04 0.43 1.50E+04 NA

83

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 3.37E-03 64.8 0.7 0.12 1.24 3.78E-03 4.52E-04 0.34 3.70E-03 68.6

51 9 45.8 0 0 0 0 0.00E+00 NA

2 3.42E-03 64.9 0.26 0 0 0 3.64E-03

52 1 45.8 0 0 0 0 0.00E+00 NA

2 3.42E-03 64.9 0.26 0 0 0 3.64E-03

52 2 46.5 2188 2.11 0.3 0.1 1.50E-02 3.64E-05 0.42 1.55E+04 NA

2 3.47E-03 64.9 0.73 0.13 1.04 3.79E-03 3.69E-04 0.34 3.58E-03 84.4

52 3 47.2 2579 2.98 0.5 0.27 1.51E-02 6.71E-05 0.43 1.86E+04 NA

2 3.52E-03 65 1.01 0.21 1.35 3.75E-03 3.38E-04 0.4 3.53E-03 78.8

52 4 47.9 2979 4.19 0.79 -0.06 1.56E-02 -1.05E-05 0.44 2.18E+04 NA

2 3.57E-03 65 1.4 0.35 1.7 3.82E-03 3.15E-04 0.47 3.48E-03 91.9

52 5 48.7 3371 5.52 1.23 -0.05 1.58E-02 -6.68E-06 0.43 2.51E+04 NA

2 3.63E-03 65.1 1.91 0.53 2.5 4.01E-03 3.56E-04 0.53 3.42E-03 91.1

52 6 49.3 2980 4.41 0.83 0.05 1.60E-02 9.69E-06 0.45 2.24E+04 NA

2 3.68E-03 65.1 1.45 0.38 2.06 3.85E-03 3.71E-04 0.47 3.38E-03 88.5

52 7 49.9 2579 3.19 0.53 0.36 1.52E-02 8.54E-05 0.43 1.96E+04 NA

2 3.72E-03 65.1 1.08 0.23 1.28 3.78E-03 3.05E-04 0.4 3.34E-03 74.3

52 8 50.5 2184 2.38 0.33 0.29 1.56E-02 9.39E-05 0.44 1.69E+04 NA

2 3.77E-03 65.2 0.8 0.15 1.42 3.86E-03 4.64E-04 0.34 3.30E-03 78.6

52 9 51.2 0 0 0 0 0.00E+00 NA

2 3.82E-03 65.2 0.24 0 0 0 3.25E-03

53 1 51.2 0 0 0 0 0.00E+00 NA

2 3.82E-03 65.2 0.24 0 0 0 3.25E-03

53 2 52.2 2185 2.47 0.35 0.2 1.57E-02 6.40E-05 0.44 1.74E+04 NA

2 3.89E-03 65.3 0.83 0.15 1.13 3.88E-03 3.58E-04 0.34 3.19E-03 79.9

53 3 52.8 2582 3.52 0.57 0.3 1.59E-02 6.80E-05 0.46 2.08E+04 NA

2 3.93E-03 65.3 1.15 0.26 1.46 3.79E-03 3.27E-04 0.4 3.16E-03 78.3

53 4 53.4 2975 4.91 0.9 -0.16 1.65E-02 -2.62E-05 0.47 2.43E+04 NA

2 3.98E-03 65.4 1.59 0.42 2.21 3.89E-03 3.69E-04 0.47 3.12E-03 94.1

53 5 54.1 3365 6.41 1.34 -0.05 1.66E-02 -6.18E-06 0.47 2.78E+04 NA

2 4.04E-03 65.4 2.08 0.63 3.02 3.94E-03 3.89E-04 0.53 3.08E-03 90.9

84

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

53 6 54.8 2973 5.06 0.9 0.11 1.66E-02 1.85E-05 0.48 2.49E+04 NA

2 4.09E-03 65.5 1.6 0.44 2.76 3.83E-03 4.50E-04 0.46 3.04E-03 87.6

53 7 56 2546 3.65 0.57 0.19 1.60E-02 4.02E-05 0.46 2.18E+04 NA

2 4.17E-03 65.5 1.18 0.27 1.83 3.78E-03 3.98E-04 0.4 2.98E-03 84.2

53 8 56.8 2183 2.71 0.37 0.18 1.59E-02 5.25E-05 0.45 1.89E+04 NA

2 4.23E-03 65.6 0.89 0.17 1.69 3.81E-03 4.92E-04 0.34 2.93E-03 83.9

53 9 57.6 0 0 0 0 0.00E+00 NA

2 4.29E-03 65.6 0.25 0 0 0 2.89E-03

54 1 13.5 0 0 0 0 0.00E+00 NA

2 1.01E-03 64.1 0.25 0 0 0 1.26E-02

54 2 14.4 2190 0.66 0.11 0.48 1.52E-02 5.48E-04 0.38 4.75E+03 NA

2 1.08E-03 64.1 0.25 0.04 -0.18 4.22E-03 -2.02E-04 0.34 1.17E-02 -20.3

54 3 15 2586 0.9 0.17 0.62 1.42E-02 4.87E-04 0.36 5.84E+03 NA

2 1.12E-03 64.2 0.36 0.06 -0.33 4.10E-03 -2.58E-04 0.4 1.13E-02 -27.9

54 4 15.7 2979 1.33 0.26 0.36 1.51E-02 2.02E-04 0.41 7.03E+03 NA

2 1.17E-03 64.3 0.47 0.11 0.35 3.88E-03 1.95E-04 0.47 1.08E-02 44.1

54 5 16.4 3366 1.63 0.4 0.58 1.39E-02 2.45E-04 0.37 8.33E+03 NA

2 1.23E-03 64.4 0.62 0.15 0.48 3.87E-03 2.03E-04 0.53 1.03E-02 39.6

54 6 17.2 0 0 0 0 0.00E+00 NA

2 1.29E-03 64.4 0.26 0 0 0 9.79E-03

55 1 21.9 0 0 0 0 0.00E+00 NA

2 1.63E-03 65.1 0.24 0 0 0 7.71E-03

55 2 22.7 2182 1 0.15 0.37 1.46E-02 2.67E-04 0.4 7.50E+03 NA

2 1.70E-03 65.2 0.36 0.06 -0.13 3.87E-03 -9.72E-05 0.34 7.40E-03 -20

55 3 23.4 2577 1.43 0.24 0.39 1.46E-02 1.97E-04 0.41 9.12E+03 NA

2 1.74E-03 65.3 0.5 0.1 0 3.70E-03 1.56E-06 0.4 7.20E-03 0.5

55 4 23.9 2975 2.01 0.39 0.13 1.50E-02 4.85E-05 0.42 1.08E+04 NA

2 1.78E-03 65.4 0.7 0.17 0.72 3.81E-03 2.67E-04 0.46 7.04E-03 79.7

55 5 24.4 3368 2.56 0.6 0.46 1.47E-02 1.31E-04 0.4 1.25E+04 NA

2 1.82E-03 65.4 0.93 0.24 0.66 3.89E-03 1.88E-04 0.53 6.88E-03 55.1

55 6 25.1 2975 2.1 0.4 0.46 1.50E-02 1.65E-04 0.43 1.13E+04 NA 85

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 1.87E-03 65.5 0.71 0.17 0.51 3.72E-03 1.80E-04 0.46 6.70E-03 47.5

55 7 25.7 2582 1.56 0.26 0.57 1.45E-02 2.62E-04 0.41 1.00E+04 NA

2 1.91E-03 65.5 0.54 0.11 0.2 3.65E-03 9.04E-05 0.4 6.55E-03 19

55 8 26.2 2184 1.1 0.17 0.71 1.40E-02 4.47E-04 0.38 8.66E+03 NA

2 1.95E-03 65.6 0.4 0.06 0.21 3.73E-03 1.31E-04 0.34 6.42E-03 16.3

55 9 26.8 0 0 0 0 0.00E+00 NA

2 2.00E-03 65.6 0.24 0 0 0 6.26E-03

56 1 26.8 0 0 0 0 0.00E+00 NA

2 2.00E-03 65.6 0.24 0 0 0 6.26E-03

56 2 27.5 2184 1.1 0.18 0.41 1.33E-02 2.48E-04 0.35 9.12E+03 NA

2 2.05E-03 65.7 0.43 0.06 0.2 3.77E-03 1.19E-04 0.34 6.10E-03 25.7

56 3 28.2 2578 1.67 0.29 0.38 1.41E-02 1.59E-04 0.4 1.10E+04 NA

2 2.10E-03 65.8 0.59 0.12 0.44 3.65E-03 1.85E-04 0.4 5.96E-03 49.4

56 4 28.7 2976 2.34 0.46 0.13 1.46E-02 3.92E-05 0.41 1.29E+04 NA

2 2.14E-03 65.8 0.81 0.19 0.92 3.70E-03 2.87E-04 0.46 5.85E-03 82.2

56 5 29.3 3367 3.02 0.72 0.39 1.44E-02 9.17E-05 0.38 1.50E+04 NA

2 2.19E-03 65.9 1.12 0.28 1.17 3.92E-03 2.77E-04 0.53 5.72E-03 71.7

56 6 29.8 2971 2.48 0.5 0.21 1.49E-02 6.32E-05 0.41 1.34E+04 NA

2 2.22E-03 65.9 0.88 0.2 1.1 3.88E-03 3.29E-04 0.46 5.62E-03 79.1

56 7 30.5 2580 1.79 0.32 0.66 1.40E-02 2.57E-04 0.39 1.19E+04 NA

2 2.27E-03 65.9 0.64 0.12 0.55 3.69E-03 2.12E-04 0.4 5.51E-03 39.6

56 8 31 2182 1.22 0.2 0.64 1.32E-02 3.44E-04 0.35 1.03E+04 NA

2 2.31E-03 65.9 0.47 0.07 0.44 3.72E-03 2.36E-04 0.34 5.41E-03 34.5

56 9 31.6 0 0 0 0 0.00E+00 NA

2 2.35E-03 66 0.26 0 0 0 5.31E-03

57 1 31.6 0 0 0 0 0.00E+00 NA

2 2.35E-03 66 0.26 0 0 0 5.31E-03

57 2 32.4 2183 1.3 0.21 0.5 1.34E-02 2.54E-04 0.36 1.07E+04 NA

2 2.41E-03 66.1 0.5 0.07 0.33 3.77E-03 1.67E-04 0.34 5.18E-03 33.3

57 3 33.1 2579 2 0.34 0.32 1.44E-02 1.14E-04 0.41 1.30E+04 NA

2 2.47E-03 66.2 0.7 0.14 0.66 3.70E-03 2.36E-04 0.4 5.07E-03 64.2

86

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

57 4 33.7 2972 2.89 0.55 -0.03 1.54E-02 -7.91E-06 0.44 1.52E+04 NA

2 2.51E-03 66.2 0.97 0.24 1.29 3.76E-03 3.40E-04 0.46 4.97E-03 91.3

57 5 34.4 3367 3.71 0.85 0.31 1.51E-02 6.37E-05 0.41 1.76E+04 NA

2 2.56E-03 66.3 1.32 0.35 1.61 3.93E-03 3.25E-04 0.53 4.88E-03 78.9

57 6 35.9 2976 3.19 0.58 0.21 1.59E-02 5.19E-05 0.46 1.62E+04 NA

2 2.67E-03 66.4 1.03 0.27 1.62 3.76E-03 4.01E-04 0.46 4.67E-03 82.6

57 7 36.6 2579 2.28 0.38 0.51 1.49E-02 1.65E-04 0.43 1.43E+04 NA

2 2.72E-03 66.4 0.77 0.16 1 3.70E-03 3.25E-04 0.4 4.58E-03 63

57 8 37.3 2182 1.57 0.24 0.59 1.40E-02 2.62E-04 0.39 1.23E+04 NA

2 2.77E-03 66.4 0.57 0.09 0.64 3.73E-03 2.87E-04 0.34 4.50E-03 47.6

57 9 38 0 0 0 0 0.00E+00 NA

2 2.83E-03 66.5 0.23 0 0 0 4.41E-03

58 1 38 0 0 0 0 0.00E+00 NA

2 2.83E-03 66.5 0.23 0 0 0 4.41E-03

58 2 38.8 2184 1.68 0.25 0.23 1.44E-02 9.80E-05 0.39 1.29E+04 NA

2 2.88E-03 66.6 0.61 0.1 0.6 3.81E-03 2.56E-04 0.34 4.32E-03 69

58 3 39.5 2582 2.5 0.41 0.15 1.51E-02 4.36E-05 0.43 1.55E+04 NA

2 2.94E-03 66.6 0.84 0.18 0.97 3.72E-03 2.90E-04 0.4 4.24E-03 81.4

58 4 40.1 2975 3.41 0.65 -0.2 1.53E-02 -4.36E-05 0.43 1.81E+04 NA

2 2.98E-03 66.7 1.15 0.28 1.18 3.77E-03 2.62E-04 0.46 4.18E-03 99.4

58 5 40.8 3367 4.45 1 0.09 1.53E-02 1.56E-05 0.42 2.09E+04 NA

2 3.03E-03 66.7 1.56 0.42 1.72 3.93E-03 2.94E-04 0.53 4.11E-03 87

58 6 41.4 2976 3.6 0.68 -0.03 1.56E-02 -6.43E-06 0.44 1.87E+04 NA

2 3.08E-03 66.7 1.2 0.3 1.57 3.80E-03 3.38E-04 0.46 4.04E-03 91.1

58 7 42.1 2577 2.69 0.44 0.09 1.53E-02 2.41E-05 0.44 1.65E+04 NA

2 3.13E-03 66.7 0.9 0.19 1.07 3.73E-03 3.01E-04 0.4 3.98E-03 85.4

58 8 42.7 2183 1.83 0.28 0.35 1.43E-02 1.34E-04 0.39 1.42E+04 NA

2 3.17E-03 66.7 0.66 0.11 0.62 3.80E-03 2.40E-04 0.34 3.93E-03 60.7

58 9 43.3 0 0 0 0 0.00E+00 NA

2 3.22E-03 66.8 0.23 0 0 0 3.86E-03

59 1 43.3 0 0 0 0 0.00E+00 NA 87

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 3.22E-03 66.8 0.23 0 0 0 3.86E-03

59 2 44.4 2183 1.94 0.29 0.42 1.46E-02 1.58E-04 0.4 1.47E+04 NA

2 3.30E-03 66.8 0.7 0.12 0.63 3.86E-03 2.34E-04 0.34 3.77E-03 56

59 3 45 2584 2.95 0.48 0.14 1.57E-02 3.80E-05 0.45 1.77E+04 NA

2 3.34E-03 66.8 0.97 0.22 1.29 3.75E-03 3.40E-04 0.4 3.72E-03 83.6

59 4 45.7 2974 4.01 0.75 -0.12 1.58E-02 -2.43E-05 0.45 2.06E+04 NA

2 3.39E-03 66.9 1.32 0.34 2.08 3.81E-03 4.07E-04 0.46 3.67E-03 93.4

59 5 46.3 3370 5.25 1.16 0.09 1.59E-02 1.34E-05 0.43 2.37E+04 NA

2 3.44E-03 66.9 1.81 0.5 2.37 3.99E-03 3.56E-04 0.53 3.62E-03 87.8

59 6 46.9 2973 4.2 0.78 -0.1 1.61E-02 -1.88E-05 0.46 2.12E+04 NA

2 3.49E-03 66.9 1.37 0.36 2.05 3.84E-03 3.91E-04 0.46 3.57E-03 92.8

59 7 47.6 2577 3.19 0.5 0.01 1.61E-02 3.63E-06 0.47 1.87E+04 NA

2 3.54E-03 67 1.02 0.24 1.59 3.76E-03 3.97E-04 0.4 3.52E-03 89.5

59 8 48.4 2183 2.15 0.31 0.39 1.48E-02 1.33E-04 0.41 1.61E+04 NA

2 3.60E-03 67 0.75 0.13 1.1 3.79E-03 3.78E-04 0.34 3.46E-03 70.6

59 9 49 0 0 0 0 0.00E+00 NA

2 3.64E-03 67 0.24 0 0 0 3.42E-03

60 1 49 0 0 0 0 0.00E+00 NA

2 3.64E-03 67 0.24 0 0 0 3.42E-03

60 2 50.2 2184 2.28 0.33 0.31 1.52E-02 1.02E-04 0.42 1.67E+04 NA

2 3.73E-03 67.1 0.79 0.14 1.09 3.82E-03 3.61E-04 0.34 3.34E-03 74.3

60 3 50.8 2578 3.46 0.54 -0.13 1.63E-02 -2.96E-05 0.48 1.99E+04 NA

2 3.77E-03 67.1 1.1 0.26 1.63 3.79E-03 3.83E-04 0.4 3.30E-03 94.4

60 4 51.5 2972 4.7 0.85 -0.4 1.64E-02 -6.94E-05 0.47 2.33E+04 NA

2 3.83E-03 67.2 1.51 0.4 2.09 3.85E-03 3.63E-04 0.46 3.25E-03 100.8

60 5 52.2 3367 6.06 1.29 -0.2 1.63E-02 -2.68E-05 0.46 2.67E+04 NA

2 3.88E-03 67.2 2.01 0.59 2.65 3.95E-03 3.55E-04 0.53 3.21E-03 94.3

60 6 53.4 2976 4.9 0.89 -0.32 1.65E-02 -5.42E-05 0.48 2.42E+04 NA

2 3.97E-03 67.2 1.56 0.42 2.18 3.85E-03 3.65E-04 0.46 3.14E-03 98.5

60 7 54 2581 3.67 0.57 -0.07 1.63E-02 -1.44E-05 0.47 2.12E+04 NA

2 4.01E-03 67.3 1.17 0.27 1.71 3.79E-03 3.76E-04 0.4 3.10E-03 92.2

60 8 54.5 2183 2.45 0.35 0.29 1.50E-02 8.93E-05 0.42 1.81E+04 NA

88

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 4.05E-03 67.3 0.85 0.15 1.03 3.82E-03 3.14E-04 0.34 3.07E-03 74.1

60 9 55.2 0 0 0 0 0.00E+00 NA

2 4.10E-03 67.3 0.24 0 0 0 3.03E-03

61 1 55.2 0 0 0 0 0.00E+00 NA

2 4.10E-03 67.3 0.24 0 0 0 3.03E-03

61 2 55.9 2190 2.56 0.38 0.37 1.52E-02 1.09E-04 0.41 1.86E+04 NA

2 4.15E-03 67.3 0.91 0.16 1.11 3.94E-03 3.28E-04 0.34 3.00E-03 71.6

61 3 57.3 2582 3.96 0.62 -0.17 1.65E-02 -3.57E-05 0.48 2.25E+04 NA

2 4.25E-03 67.4 1.26 0.3 1.85 3.83E-03 3.83E-04 0.4 2.92E-03 95.3

61 4 58.2 2971 5.42 0.97 -0.19 1.68E-02 -2.93E-05 0.48 2.63E+04 NA

2 4.32E-03 67.5 1.72 0.47 2.43 3.90E-03 3.75E-04 0.46 2.87E-03 94.5

61 5 59 3365 7.13 1.46 -0.63 1.70E-02 -7.42E-05 0.48 3.02E+04 NA

2 4.38E-03 67.6 2.28 0.71 3.46 3.98E-03 4.11E-04 0.52 2.84E-03 100.2

61 6 59.7 2975 5.62 0.99 -0.31 1.70E-02 -4.66E-05 0.5 2.70E+04 NA

2 4.43E-03 67.6 1.75 0.49 2.5 3.86E-03 3.75E-04 0.46 2.81E-03 97.1

61 7 60.3 2580 4.17 0.65 -0.13 1.66E-02 -2.47E-05 0.49 2.36E+04 NA

2 4.47E-03 67.6 1.31 0.31 1.92 3.81E-03 3.79E-04 0.4 2.78E-03 93.7

61 8 61.1 2184 2.82 0.4 0.3 1.54E-02 8.13E-05 0.43 2.03E+04 NA

2 4.54E-03 67.7 0.96 0.17 1.24 3.83E-03 3.36E-04 0.34 2.74E-03 76.4

61 9 61.9 0 0 0 0 0.00E+00 NA

2 4.60E-03 67.7 0.24 0 0 0 2.70E-03

62 1 61.9 0 0 0 0 0.00E+00 NA

2 4.60E-03 67.7 0.24 0 0 0 2.70E-03

62 2 62.7 2183 2.89 0.42 0.57 1.54E-02 1.50E-04 0.43 2.08E+04 NA

2 4.65E-03 67.7 1 0.18 1.32 3.89E-03 3.50E-04 0.34 2.67E-03 66.7

62 3 63.4 2577 4.46 0.68 -0.14 1.69E-02 -2.71E-05 0.49 2.48E+04 NA

2 4.70E-03 67.8 1.39 0.34 2.11 3.84E-03 3.97E-04 0.4 2.64E-03 93.9

62 4 64 2972 6.15 1.08 -0.39 1.73E-02 -5.52E-05 0.5 2.89E+04 NA

2 4.75E-03 67.8 1.9 0.54 2.85 3.91E-03 3.99E-04 0.46 2.61E-03 97.9

62 5 64.7 3369 7.88 1.6 -0.31 1.71E-02 -3.33E-05 0.49 3.31E+04 NA

2 4.80E-03 67.8 2.49 0.78 3.89 3.96E-03 4.20E-04 0.53 2.59E-03 94.5 89

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

62 6 65.2 2978 6.35 1.1 -0.45 1.75E-02 -6.20E-05 0.51 2.95E+04 NA

2 4.84E-03 67.8 1.94 0.56 2.93 3.90E-03 4.01E-04 0.46 2.57E-03 98.8

62 7 65.9 2579 4.63 0.71 -0.38 1.68E-02 -6.94E-05 0.49 2.58E+04 NA

2 4.89E-03 67.9 1.44 0.35 2.02 3.82E-03 3.65E-04 0.4 2.54E-03 100.7

62 8 66.7 2183 3.1 0.44 0.36 1.55E-02 9.06E-05 0.43 2.21E+04 NA

2 4.95E-03 67.9 1.06 0.19 1.27 3.87E-03 3.15E-04 0.34 2.51E-03 74

62 9 67.4 0 0 0 0 0.00E+00 NA

2 5.00E-03 67.9 0.25 0 0 0 2.48E-03

63 1 67.4 0 0 0 0 0.00E+00 NA

2 5.00E-03 67.9 0.25 0 0 0 2.48E-03

63 2 68.2 2186 3.16 0.45 0.34 1.55E-02 8.31E-05 0.43 2.26E+04 NA

2 5.06E-03 67.9 1.08 0.19 1.33 3.88E-03 3.24E-04 0.34 2.46E-03 75.6

63 3 68.9 2581 4.9 0.74 -0.38 1.70E-02 -6.61E-05 0.5 2.71E+04 NA

2 5.11E-03 68 1.51 0.37 2.28 3.83E-03 3.94E-04 0.4 2.43E-03 99.5

63 4 69.5 2975 6.7 1.17 -0.7 1.73E-02 -9.07E-05 0.51 3.14E+04 NA

2 5.15E-03 68 2.06 0.59 3.53 3.91E-03 4.54E-04 0.46 2.41E-03 101.3

63 5 69.8 3365 8.71 1.75 -1.06 1.75E-02 -1.06E-04 0.5 3.57E+04 NA

2 5.18E-03 68 2.73 0.88 4.49 4.02E-03 4.50E-04 0.52 2.40E-03 103.3

63 6 70.8 3365 8.81 1.76 -0.88 1.75E-02 -8.69E-05 0.5 3.62E+04 NA

2 5.25E-03 68.1 2.75 0.88 4.36 3.99E-03 4.30E-04 0.52 2.36E-03 101.4

63 7 71.6 2972 6.98 1.19 -1.08 1.76E-02 -1.35E-04 0.52 3.24E+04 NA

2 5.31E-03 68.1 2.11 0.62 3.47 3.89E-03 4.34E-04 0.46 2.34E-03 107.2

63 8 72.3 2581 5.16 0.78 -0.46 1.71E-02 -7.52E-05 0.5 2.84E+04 NA

2 5.36E-03 68.1 1.59 0.39 2.51 3.84E-03 4.13E-04 0.4 2.32E-03 100.3

63 9 72.9 2973 7.14 1.22 -0.94 1.77E-02 -1.16E-04 0.52 3.29E+04 NA

2 5.41E-03 68.1 2.16 0.64 3.16 3.90E-03 3.88E-04 0.46 2.30E-03 106.6

63 10 75.2 2184 3.5 0.5 0.16 1.55E-02 3.64E-05 0.43 2.50E+04 NA

2 5.58E-03 68.2 1.19 0.21 1.52 3.88E-03 3.37E-04 0.34 2.23E-03 83.8

63 11 76 0 0 0 0 0.00E+00 NA

2 5.64E-03 68.3 0.25 0 0 0 2.20E-03

64 1 76 0 0 0 0 0.00E+00 NA

90

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 5.64E-03 68.3 0.25 0 0 0 2.20E-03

64 2 76.9 2182 3.63 0.52 0.44 1.58E-02 9.56E-05 0.44 2.55E+04 NA

2 5.70E-03 68.3 1.24 0.23 1.77 3.95E-03 3.83E-04 0.34 2.18E-03 76

64 3 77.5 2579 5.69 0.85 -0.65 1.76E-02 -9.93E-05 0.52 3.04E+04 NA

2 5.75E-03 68.3 1.73 0.44 2.8 3.91E-03 4.30E-04 0.4 2.16E-03 103

64 4 78.4 2965 7.78 1.32 -1.4 1.80E-02 -1.61E-04 0.53 3.54E+04 NA

2 5.81E-03 68.4 2.34 0.7 4.12 3.95E-03 4.74E-04 0.46 2.14E-03 108.8

64 5 79 3367 10.23 1.98 -1.55 1.82E-02 -1.37E-04 0.53 4.04E+04 NA

2 5.86E-03 68.4 3.09 1.05 5.62 4.03E-03 4.98E-04 0.52 2.12E-03 105.4

64 6 79.5 2972 7.99 1.34 -1.46 1.81E-02 -1.65E-04 0.54 3.59E+04 NA

2 5.89E-03 68.4 2.37 0.72 4.51 3.94E-03 5.09E-04 0.46 2.11E-03 107.9

64 7 80 2579 5.86 0.87 -0.67 1.76E-02 -9.94E-05 0.52 3.14E+04 NA

2 5.93E-03 68.4 1.78 0.45 3.06 3.89E-03 4.56E-04 0.4 2.09E-03 102.3

64 8 80.8 2183 3.9 0.54 0.1 1.61E-02 2.07E-05 0.45 2.68E+04 NA

2 5.99E-03 68.4 1.3 0.24 1.78 3.93E-03 3.67E-04 0.34 2.07E-03 86.8

64 9 81.4 0 0 0 0 0.00E+00 NA

2 6.03E-03 68.5 0.26 0 0 0 2.06E-03

65 1 81.4 0 0 0 0 0.00E+00 NA

2 6.03E-03 68.5 0.26 0 0 0 2.06E-03

65 2 82.1 2183 3.99 0.55 0.45 1.63E-02 9.18E-05 0.46 2.72E+04 NA

2 6.09E-03 68.5 1.32 0.25 1.91 3.93E-03 3.87E-04 0.34 2.04E-03 76.7

65 3 82.8 2579 6.23 0.91 -0.99 1.80E-02 -1.42E-04 0.53 3.25E+04 NA

2 6.14E-03 68.6 1.86 0.49 2.98 3.93E-03 4.29E-04 0.4 2.02E-03 108.3

65 4 83.5 2975 8.48 1.42 -1.12 1.83E-02 -1.20E-04 0.54 3.78E+04 NA

2 6.19E-03 68.6 2.5 0.77 4.47 3.95E-03 4.80E-04 0.46 2.00E-03 104.1

65 5 84.3 3369 11.08 2.13 -1.5 1.85E-02 -1.24E-04 0.54 4.32E+04 NA

2 6.24E-03 68.6 3.31 1.15 5.97 4.04E-03 4.95E-04 0.52 1.99E-03 104.1

65 6 85 2974 8.73 1.44 -1.63 1.85E-02 -1.72E-04 0.55 3.84E+04 NA

2 6.30E-03 68.6 2.55 0.8 4.62 3.96E-03 4.87E-04 0.46 1.97E-03 109.5

65 7 85.8 2578 6.38 0.93 -0.68 1.79E-02 -9.47E-05 0.53 3.36E+04 NA

2 6.36E-03 68.6 1.9 0.5 3.19 3.88E-03 4.44E-04 0.4 1.95E-03 102

65 8 86.5 2186 4.29 0.57 -0.03 1.65E-02 -5.82E-06 0.48 2.87E+04 NA 91

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 6.41E-03 68.6 1.37 0.27 2.09 3.86E-03 4.01E-04 0.34 1.94E-03 90.8

65 9 87.2 0 0 0 0 0.00E+00 NA

2 6.46E-03 68.6 0.25 0 0 0 1.92E-03

66 1 87.2 0 0 0 0 0.00E+00 NA

2 6.46E-03 68.6 0.25 0 0 0 1.92E-03

66 2 88.1 2183 4.45 0.59 0.04 1.69E-02 7.63E-06 0.48 2.92E+04 NA

2 6.52E-03 68.6 1.43 0.28 1.87 3.98E-03 3.54E-04 0.34 1.90E-03 88.8

66 3 88.7 2581 6.77 0.98 -0.65 1.83E-02 -8.73E-05 0.55 3.48E+04 NA

2 6.57E-03 68.7 1.99 0.53 3.47 3.93E-03 4.66E-04 0.4 1.89E-03 100.6

66 4 89.8 2974 9.3 1.52 -1.09 1.87E-02 -1.08E-04 0.56 4.06E+04 NA

2 6.65E-03 68.7 2.69 0.85 4.74 3.95E-03 4.74E-04 0.46 1.87E-03 102.9

66 5 91.3 3366 12.2 2.29 -2.26 1.88E-02 -1.74E-04 0.56 4.67E+04 NA

2 6.77E-03 68.8 3.57 1.27 6.69 4.03E-03 5.13E-04 0.52 1.83E-03 108.7

66 6 92.1 2972 9.74 1.58 -2.62 1.91E-02 -2.56E-04 0.57 4.16E+04 NA

2 6.82E-03 68.8 2.8 0.9 5.46 4.01E-03 5.32E-04 0.46 1.82E-03 115.7

66 7 92.9 2582 7.1 1.02 -0.82 1.83E-02 -1.06E-04 0.55 3.65E+04 NA

2 6.88E-03 68.8 2.07 0.56 3.61 3.90E-03 4.63E-04 0.4 1.80E-03 102.8

66 8 93.5 2181 4.79 0.61 -0.26 1.72E-02 -4.58E-05 0.51 3.10E+04 NA

2 6.92E-03 68.8 1.47 0.31 2.33 3.86E-03 4.16E-04 0.34 1.79E-03 96.3

66 9 94.1 0 0 0 0 0.00E+00 NA

2 6.97E-03 68.8 0.24 0 0 0 1.78E-03

67 1 94.1 0 0 0 0 0.00E+00 NA

2 6.97E-03 68.8 0.24 0 0 0 1.78E-03

67 2 94.7 2183 4.9 0.63 -0.11 1.73E-02 -2.01E-05 0.5 3.14E+04 NA

2 7.02E-03 68.9 1.52 0.32 2.47 3.94E-03 4.35E-04 0.34 1.77E-03 92.6

67 3 95.5 2576 7.39 1.04 -1.35 1.86E-02 -1.69E-04 0.56 3.74E+04 NA

2 7.08E-03 68.9 2.13 0.59 4.02 3.92E-03 5.03E-04 0.4 1.75E-03 108.6

67 4 96.1 2971 10.23 1.66 -2.01 1.92E-02 -1.88E-04 0.57 4.34E+04 NA

2 7.12E-03 68.9 2.93 0.95 5.74 4.03E-03 5.37E-04 0.46 1.74E-03 109.3

67 5 96.8 3370 13.34 2.46 -2.71 1.94E-02 -1.96E-04 0.57 4.96E+04 NA

2 7.17E-03 69 3.84 1.41 7.31 4.08E-03 5.27E-04 0.52 1.73E-03 110.3

92

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

67 6 97.5 2972 10.36 1.66 -2.43 1.92E-02 -2.24E-04 0.58 4.40E+04 NA

2 7.22E-03 69 2.93 0.96 6.06 3.97E-03 5.58E-04 0.46 1.72E-03 111.9

67 7 98.1 2577 7.56 1.06 -1.32 1.85E-02 -1.61E-04 0.56 3.84E+04 NA

2 7.26E-03 69 2.17 0.6 4.61 3.88E-03 5.62E-04 0.4 1.71E-03 106

67 8 98.8 2186 5.16 0.65 -0.51 1.75E-02 -8.60E-05 0.51 3.28E+04 NA

2 7.31E-03 69 1.57 0.34 2.73 3.89E-03 4.59E-04 0.34 1.70E-03 100.6

67 9 99.3 0 0 0 0 0.00E+00 NA

2 7.36E-03 69 0.23 0 0 0 1.69E-03

68 1 99.3 0 0 0 0 0.00E+00 NA

2 7.36E-03 69 0.23 0 0 0 1.69E-03

68 2 100.1 2184 5.24 0.67 -0.14 1.75E-02 -2.35E-05 0.51 3.32E+04 NA

2 7.41E-03 69 1.62 0.34 3.03 3.96E-03 5.04E-04 0.34 1.67E-03 92.7

68 3 100.8 2577 7.96 1.11 -1.42 1.90E-02 -1.69E-04 0.57 3.95E+04 NA

2 7.46E-03 69.1 2.27 0.64 4.51 3.95E-03 5.34E-04 0.4 1.66E-03 107.5

68 4 101.5 2975 10.63 1.73 -1.97 1.89E-02 -1.74E-04 0.57 4.59E+04 NA

2 7.51E-03 69.1 3.05 0.98 5.77 3.97E-03 5.10E-04 0.46 1.65E-03 108.8

68 5 102.1 3370 14.04 2.61 -2.65 1.93E-02 -1.81E-04 0.57 5.23E+04 NA

2 7.56E-03 69.2 4.07 1.48 7.22 4.10E-03 4.94E-04 0.52 1.64E-03 110.1

68 6 102.8 2973 11 1.74 -2.45 1.93E-02 -2.14E-04 0.59 4.65E+04 NA

2 7.61E-03 69.2 3.08 1.03 5.59 3.95E-03 4.88E-04 0.46 1.63E-03 113.7

68 7 103.6 2583 8.14 1.14 -1.69 1.88E-02 -1.94E-04 0.57 4.07E+04 NA

2 7.67E-03 69.2 2.31 0.65 4.29 3.91E-03 4.92E-04 0.4 1.62E-03 111.5

68 8 104.2 2185 5.47 0.69 -0.66 1.75E-02 -1.06E-04 0.52 3.46E+04 NA

2 7.72E-03 69.2 1.66 0.36 2.89 3.88E-03 4.61E-04 0.34 1.61E-03 102.9

68 9 104.8 0 0 0 0 0.00E+00 NA

2 7.76E-03 69.2 0.25 0 0 0 1.60E-03

69 1 104.8 0 0 0 0 0.00E+00 NA

2 7.76E-03 69.2 0.25 0 0 0 1.60E-03

69 2 105.5 2185 5.64 0.72 -0.34 1.79E-02 -5.31E-05 0.52 3.50E+04 NA

2 7.81E-03 69.2 1.73 0.37 2.88 4.01E-03 4.55E-04 0.34 1.59E-03 96.7

69 3 106.1 2579 8.33 1.16 -0.8 1.89E-02 -9.05E-05 0.57 4.16E+04 NA

93

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 7.85E-03 69.3 2.36 0.67 4.28 3.91E-03 4.82E-04 0.4 1.58E-03 100.6

69 4 106.8 2972 11.26 1.83 -1.19 1.91E-02 -1.00E-04 0.57 4.82E+04 NA

2 7.90E-03 69.3 3.23 1.04 5.11 4.00E-03 4.31E-04 0.46 1.57E-03 103.1

69 5 107.4 3370 14.81 2.73 -2.89 1.94E-02 -1.88E-04 0.58 5.50E+04 NA

2 7.95E-03 69.3 4.25 1.57 6.96 4.07E-03 4.53E-04 0.52 1.56E-03 112.5

69 6 108 2978 11.68 1.85 -2.24 1.95E-02 -1.86E-04 0.59 4.89E+04 NA

2 7.99E-03 69.3 3.26 1.1 6.15 3.98E-03 5.10E-04 0.46 1.55E-03 110

69 7 108.6 2579 8.53 1.18 -1.58 1.89E-02 -1.73E-04 0.58 4.26E+04 NA

2 8.04E-03 69.4 2.41 0.68 4.51 3.89E-03 4.96E-04 0.4 1.54E-03 109.3

69 8 109.3 2184 5.83 0.72 -0.54 1.79E-02 -8.26E-05 0.53 3.63E+04 NA

2 8.08E-03 69.4 1.74 0.38 3.12 3.90E-03 4.76E-04 0.34 1.53E-03 99.9

69 9 109.9 0 0 0 0 0.00E+00 NA

2 8.13E-03 69.4 0.26 0 0 0 1.53E-03

70 1 109.9 0 0 0 0 0.00E+00 NA

2 8.13E-03 69.4 0.26 0 0 0 1.53E-03

70 2 110.5 2186 5.93 0.74 -0.22 1.79E-02 -3.34E-05 0.53 3.67E+04 NA

2 8.18E-03 69.4 1.78 0.39 3.21 3.93E-03 4.83E-04 0.34 1.52E-03 94

70 3 112.1 2578 8.88 1.22 -1.62 1.90E-02 -1.73E-04 0.58 4.39E+04 NA

2 8.29E-03 69.4 2.49 0.71 4.46 3.90E-03 4.76E-04 0.4 1.50E-03 110

70 4 112.9 2971 12.1 1.94 -2.5 1.94E-02 -2.00E-04 0.58 5.10E+04 NA

2 8.35E-03 69.5 3.43 1.13 6.75 4.02E-03 5.38E-04 0.46 1.48E-03 110.4

70 5 113.7 3366 16.04 2.88 -4 1.99E-02 -2.47E-04 0.6 5.81E+04 NA

2 8.41E-03 69.5 4.49 1.72 8.57 4.08E-03 5.28E-04 0.52 1.47E-03 115

70 6 114.3 2974 12.44 1.95 -2.79 1.97E-02 -2.19E-04 0.6 5.17E+04 NA

2 8.46E-03 69.5 3.45 1.17 6.61 3.99E-03 5.19E-04 0.46 1.47E-03 112.9

70 7 115.2 2576 9.24 1.26 -2.01 1.93E-02 -2.08E-04 0.59 4.51E+04 NA

2 8.52E-03 69.5 2.57 0.75 4.68 3.92E-03 4.86E-04 0.4 1.45E-03 113.2

70 8 116 2183 6.25 0.76 -0.61 1.80E-02 -8.73E-05 0.54 3.85E+04 NA

2 8.58E-03 69.5 1.84 0.41 3.4 3.89E-03 4.88E-04 0.34 1.44E-03 100.1

70 9 116.6 0 0 0 0 0.00E+00 NA

2 8.63E-03 69.5 0.26 0 0 0 1.44E-03

94

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

71 1 116.6 0 0 0 0 0.00E+00 NA

2 8.63E-03 69.5 0.26 0 0 0 1.44E-03

71 2 117.5 2181 6.39 0.78 -0.43 1.83E-02 -6.15E-05 0.54 3.89E+04 NA

2 8.69E-03 69.5 1.88 0.42 3.06 3.93E-03 4.35E-04 0.34 1.43E-03 98

71 3 118.1 2576 9.48 1.28 -1.58 1.93E-02 -1.60E-04 0.6 4.62E+04 NA

2 8.74E-03 69.6 2.62 0.77 5.32 3.91E-03 5.39E-04 0.4 1.42E-03 106.6

71 4 118.9 2974 13.05 2.04 -3.04 1.98E-02 -2.30E-04 0.6 5.37E+04 NA

2 8.79E-03 69.6 3.6 1.23 6.47 4.00E-03 4.89E-04 0.46 1.41E-03 115.2

71 5 119.6 3366 17.06 3.05 -3.82 2.01E-02 -2.24E-04 0.6 6.12E+04 NA

2 8.85E-03 69.6 4.76 1.84 8.98 4.10E-03 5.26E-04 0.52 1.40E-03 113.1

71 6 120.3 2971 13.24 2.04 -2.9 1.99E-02 -2.17E-04 0.61 5.43E+04 NA

2 8.90E-03 69.6 3.61 1.25 7.01 3.98E-03 5.24E-04 0.46 1.39E-03 112.4

71 7 120.9 2580 9.83 1.32 -1.69 1.95E-02 -1.67E-04 0.6 4.74E+04 NA

2 8.94E-03 69.7 2.69 0.8 5.15 3.91E-03 5.08E-04 0.4 1.39E-03 108.2

71 8 121.6 2185 6.7 0.81 -1.09 1.85E-02 -1.49E-04 0.56 4.04E+04 NA

2 8.99E-03 69.7 1.94 0.45 3.16 3.91E-03 4.33E-04 0.34 1.38E-03 108.9

71 9 122.4 0 0 0 0 0.00E+00 NA

2 9.05E-03 69.7 0.27 0 0 0 1.37E-03

72 1 122.4 0 0 0 0 0.00E+00 NA

2 9.05E-03 69.7 0.27 0 0 0 1.37E-03

72 2 123.3 2185 6.81 0.83 -0.74 1.85E-02 -1.01E-04 0.55 4.09E+04 NA

2 9.12E-03 69.7 2 0.46 3.54 3.96E-03 4.78E-04 0.34 1.36E-03 101.9

72 3 124 2583 10.21 1.38 -2.44 1.97E-02 -2.34E-04 0.61 4.87E+04 NA

2 9.17E-03 69.8 2.8 0.84 5.36 3.95E-03 5.15E-04 0.4 1.35E-03 114.4

72 4 124.7 2971 13.72 2.13 -2.93 1.99E-02 -2.11E-04 0.61 5.63E+04 NA

2 9.22E-03 69.8 3.76 1.3 6.84 4.00E-03 4.94E-04 0.46 1.34E-03 113.2

72 5 125.5 3365 18.25 3.21 -4.45 2.05E-02 -2.49E-04 0.62 6.42E+04 NA

2 9.28E-03 69.8 5.01 1.99 9.96 4.12E-03 5.57E-04 0.52 1.34E-03 114.1

72 6 126.2 2971 14.03 2.14 -3.37 2.01E-02 -2.40E-04 0.62 5.69E+04 NA

2 9.33E-03 69.8 3.78 1.33 7.15 3.97E-03 5.10E-04 0.46 1.33E-03 115.2

72 7 126.8 2577 10.42 1.39 -2.26 1.98E-02 -2.13E-04 0.62 4.96E+04 NA

2 9.37E-03 69.8 2.82 0.85 5.54 3.92E-03 5.23E-04 0.4 1.32E-03 112.2

95

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

72 8 127.5 2184 7.05 0.85 -0.87 1.85E-02 -1.14E-04 0.56 4.23E+04 NA

2 9.42E-03 69.9 2.04 0.47 3.58 3.93E-03 4.68E-04 0.34 1.31E-03 103.7

72 9 128.2 0 0 0 0 0.00E+00 NA

2 9.48E-03 69.9 0.25 0 0 0 1.31E-03

73 1 128.2 0 0 0 0 0.00E+00 NA

2 9.48E-03 69.9 0.25 0 0 0 1.31E-03

73 2 129 2187 7.21 0.87 -0.9 1.87E-02 -1.15E-04 0.56 4.28E+04 NA

2 9.53E-03 69.9 2.08 0.49 3.9 3.95E-03 5.03E-04 0.34 1.30E-03 102.9

73 3 129.5 2579 10.59 1.41 -1.54 1.97E-02 -1.42E-04 0.61 5.07E+04 NA

2 9.57E-03 70 2.87 0.86 5.8 3.90E-03 5.36E-04 0.4 1.29E-03 104.8

73 4 130.3 2975 14.48 2.22 -3.27 2.01E-02 -2.25E-04 0.62 5.89E+04 NA

2 9.63E-03 70 3.91 1.38 7.77 3.97E-03 5.36E-04 0.46 1.29E-03 112.8

73 5 131.1 3366 19.17 3.33 -4.14 2.06E-02 -2.22E-04 0.63 6.70E+04 NA

2 9.69E-03 70.1 5.2 2.09 10.3 4.09E-03 5.51E-04 0.52 1.28E-03 111.9

73 6 131.9 2970 14.79 2.24 -3.17 2.03E-02 -2.17E-04 0.63 5.95E+04 NA

2 9.74E-03 70.1 3.96 1.41 7.99 3.98E-03 5.46E-04 0.46 1.27E-03 111.6

73 7 132.4 2577 10.9 1.45 -2.34 1.98E-02 -2.12E-04 0.62 5.18E+04 NA

2 9.79E-03 70.1 2.95 0.89 5.78 3.92E-03 5.22E-04 0.4 1.27E-03 112.1

73 8 133 2183 7.53 0.88 -1.1 1.90E-02 -1.38E-04 0.58 4.41E+04 NA

2 9.83E-03 70.1 2.13 0.51 4.03 3.92E-03 5.05E-04 0.34 1.26E-03 105.2

73 9 133.6 0 0 0 0 0.00E+00 NA

2 9.88E-03 70.1 0.24 0 0 0 1.25E-03

74 1 133.6 0 0 0 0 0.00E+00 NA

2 9.88E-03 70.1 0.24 0 0 0 1.25E-03

74 2 134.4 2186 7.69 0.91 -1.15 1.92E-02 -1.42E-04 0.58 4.46E+04 NA

2 9.93E-03 70.1 2.18 0.53 3.82 3.97E-03 4.73E-04 0.34 1.25E-03 106.8

74 3 135.2 2579 11.32 1.49 -2.63 2.01E-02 -2.32E-04 0.63 5.29E+04 NA

2 9.99E-03 70.2 3.04 0.94 6.23 3.95E-03 5.51E-04 0.4 1.24E-03 112.9

74 4 136.1 2973 15.12 2.35 -3.46 2.01E-02 -2.29E-04 0.61 6.14E+04 NA

2 1.01E-02 70.2 4.15 1.44 7.05 4.04E-03 4.66E-04 0.46 1.23E-03 116.1

74 5 136.6 3368 20.07 3.51 -4.63 2.07E-02 -2.38E-04 0.63 6.98E+04 NA

96

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 1.01E-02 70.2 5.48 2.2 10.4 4.14E-03 5.34E-04 0.52 1.23E-03 114

74 6 137.6 2968 15.45 2.33 -2.83 2.04E-02 -1.86E-04 0.63 6.20E+04 NA

2 1.02E-02 70.2 4.13 1.48 7.99 3.99E-03 5.24E-04 0.46 1.22E-03 109.5

74 7 138.3 2576 11.38 1.51 -1.75 1.98E-02 -1.52E-04 0.62 5.41E+04 NA

2 1.02E-02 70.2 3.07 0.93 5.77 3.91E-03 5.00E-04 0.4 1.21E-03 106.9

74 8 139 2182 7.95 0.93 -1.07 1.92E-02 -1.29E-04 0.58 4.61E+04 NA

2 1.03E-02 70.2 2.24 0.54 3.84 3.95E-03 4.61E-04 0.34 1.21E-03 105.6

74 9 139.8 0 0 0 0 0.00E+00 NA

2 1.03E-02 70.2 0.27 0 0 0 1.20E-03

75 1 139.8 0 0 0 0 0.00E+00 NA

2 1.03E-02 70.2 0.27 0 0 0 1.20E-03

75 2 140.4 2183 8.03 0.94 -0.56 1.92E-02 -6.66E-05 0.58 4.65E+04 NA

2 1.04E-02 70.2 2.26 0.55 3.67 3.95E-03 4.36E-04 0.34 1.19E-03 98.7

75 3 141 2580 11.72 1.55 -1.5 2.00E-02 -1.27E-04 0.62 5.52E+04 NA

2 1.04E-02 70.2 3.15 0.97 6.11 3.93E-03 5.18E-04 0.4 1.19E-03 103.8

75 4 141.6 2972 15.71 2.41 -1.37 2.01E-02 -8.70E-05 0.62 6.39E+04 NA

2 1.05E-02 70.3 4.26 1.49 6.75 3.98E-03 4.29E-04 0.46 1.18E-03 101.5

75 5 142.5 3366 21.25 3.68 -4.95 2.11E-02 -2.44E-04 0.64 7.28E+04 NA

2 1.05E-02 70.3 5.74 2.34 10.97 4.16E-03 5.41E-04 0.52 1.18E-03 114.3

75 6 143.1 2970 16.31 2.44 -3.5 2.07E-02 -2.20E-04 0.64 6.45E+04 NA

2 1.06E-02 70.3 4.32 1.57 8.05 4.00E-03 5.07E-04 0.46 1.17E-03 113.5

75 7 143.7 2580 11.96 1.58 -1.57 2.00E-02 -1.30E-04 0.62 5.63E+04 NA

2 1.06E-02 70.4 3.22 0.99 6.11 3.94E-03 5.09E-04 0.4 1.17E-03 104.4

75 8 144.3 2185 8.32 0.96 -0.67 1.93E-02 -7.75E-05 0.59 4.78E+04 NA

2 1.07E-02 70.4 2.31 0.57 4.14 3.92E-03 4.78E-04 0.34 1.16E-03 99.2

75 9 144.9 0 0 0 0 0.00E+00 NA

2 1.07E-02 70.4 0.28 0 0 0 1.16E-03

76 1 144.9 0 0 0 0 0.00E+00 NA

2 1.07E-02 70.4 0.28 0 0 0 1.16E-03

76 2 145.6 2181 8.37 0.98 -0.72 1.93E-02 -8.31E-05 0.58 4.82E+04 NA

2 1.08E-02 70.4 2.36 0.57 4.05 3.99E-03 4.66E-04 0.34 1.15E-03 100.1 97

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

76 3 146.4 2579 12.3 1.61 -1.97 2.02E-02 -1.61E-04 0.63 5.73E+04 NA

2 1.08E-02 70.4 3.29 1.02 6.17 3.95E-03 5.04E-04 0.4 1.15E-03 107.7

76 4 146.9 2972 16.6 2.52 -2.79 2.05E-02 -1.71E-04 0.63 6.63E+04 NA

2 1.08E-02 70.4 4.46 1.59 8.31 4.02E-03 5.10E-04 0.46 1.14E-03 108.6

76 5 147.6 3365 22.1 3.77 -4.9 2.12E-02 -2.33E-04 0.65 7.54E+04 NA

2 1.09E-02 70.4 5.88 2.44 12.2 4.12E-03 5.81E-04 0.52 1.14E-03 111.9

76 6 148.2 2975 17.01 2.54 -3.87 2.08E-02 -2.35E-04 0.65 6.69E+04 NA

2 1.09E-02 70.5 4.49 1.65 8.89 4.00E-03 5.39E-04 0.46 1.13E-03 113.5

76 7 148.9 2580 12.53 1.63 -1.94 2.02E-02 -1.56E-04 0.64 5.83E+04 NA

2 1.10E-02 70.5 3.32 1.04 6.49 3.92E-03 5.21E-04 0.4 1.13E-03 106.6

76 8 149.7 2183 8.61 0.99 -0.92 1.93E-02 -1.03E-04 0.6 4.96E+04 NA

2 1.11E-02 70.5 2.38 0.59 4.28 3.91E-03 4.77E-04 0.34 1.12E-03 102.2

76 9 150.2 0 0 0 0 0.00E+00 NA

2 1.11E-02 70.5 0.28 0 0 0 1.12E-03

77 1 150.2 0 0 0 0 0.00E+00 NA

2 1.11E-02 70.5 0.28 0 0 0 1.12E-03

77 2 150.9 2183 8.79 1.02 -1.04 1.96E-02 -1.15E-04 0.6 5.00E+04 NA

2 1.11E-02 70.5 2.45 0.61 4.66 3.98E-03 5.16E-04 0.34 1.11E-03 102.5

77 3 151.6 2577 12.76 1.67 -2.01 2.03E-02 -1.59E-04 0.63 5.93E+04 NA

2 1.12E-02 70.5 3.41 1.06 6.41 3.97E-03 5.07E-04 0.4 1.11E-03 107.4

77 4 152.2 2973 17.44 2.64 -3.99 2.08E-02 -2.36E-04 0.64 6.87E+04 NA

2 1.12E-02 70.5 4.67 1.69 8.53 4.06E-03 5.05E-04 0.46 1.10E-03 115.1

77 5 153 3367 22.9 3.89 -4.88 2.11E-02 -2.24E-04 0.65 7.82E+04 NA

2 1.13E-02 70.6 6.08 2.53 12.73 4.10E-03 5.84E-04 0.52 1.10E-03 111

77 6 153.7 2974 17.72 2.63 -4.14 2.09E-02 -2.42E-04 0.65 6.94E+04 NA

2 1.13E-02 70.6 4.65 1.72 9.46 4.00E-03 5.54E-04 0.46 1.09E-03 113.6

77 7 154.4 2576 13.05 1.69 -2.39 2.04E-02 -1.86E-04 0.64 6.04E+04 NA

2 1.14E-02 70.5 3.44 1.08 7.15 3.93E-03 5.56E-04 0.4 1.09E-03 108.5

77 8 155.1 2183 9.02 1.03 -1.56 1.95E-02 -1.68E-04 0.6 5.14E+04 NA

2 1.14E-02 70.6 2.49 0.62 4.46 3.94E-03 4.81E-04 0.34 1.08E-03 109.2

77 9 155.7 0 0 0 0 0.00E+00 NA

2 1.15E-02 70.6 0.26 0 0 0 1.08E-03

98

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

78 1 155.7 0 0 0 0 0.00E+00 NA

2 1.15E-02 70.6 0.26 0 0 0 1.08E-03

78 2 156.4 2183 9.08 1.05 -1.48 1.95E-02 -1.58E-04 0.59 5.18E+04 NA

2 1.15E-02 70.6 2.53 0.62 5 3.97E-03 5.34E-04 0.34 1.07E-03 106.5

78 3 157.1 2579 13.5 1.74 -3.21 2.07E-02 -2.45E-04 0.65 6.15E+04 NA

2 1.16E-02 70.6 3.55 1.13 6.47 3.98E-03 4.93E-04 0.4 1.07E-03 116.4

78 4 158 2976 18.23 2.74 -4.34 2.09E-02 -2.47E-04 0.65 7.13E+04 NA

2 1.17E-02 70.6 4.83 1.77 9.7 4.04E-03 5.52E-04 0.46 1.06E-03 114.1

78 5 159.1 3367 24.07 4.07 -6.09 2.14E-02 -2.69E-04 0.66 8.12E+04 NA

2 1.17E-02 70.7 6.34 2.68 13.55 4.12E-03 5.98E-04 0.52 1.06E-03 114.2

78 6 159.8 2974 18.44 2.74 -4.78 2.09E-02 -2.69E-04 0.65 7.21E+04 NA

2 1.18E-02 70.7 4.84 1.79 9.1 4.02E-03 5.13E-04 0.46 1.05E-03 117.7

78 7 160.3 2580 13.55 1.76 -2.43 2.03E-02 -1.81E-04 0.64 6.28E+04 NA

2 1.18E-02 70.7 3.59 1.12 6.91 3.94E-03 5.16E-04 0.4 1.05E-03 109.4

78 8 161.1 2185 9.24 1.07 -1.47 1.93E-02 -1.52E-04 0.59 5.34E+04 NA

2 1.19E-02 70.7 2.58 0.63 4.42 3.93E-03 4.57E-04 0.34 1.04E-03 108.4

78 9 162.1 0 0 0 0 0.00E+00 NA

2 1.20E-02 70.7 0.27 0 0 0 1.04E-03

79 1 162.1 0 0 0 0 0.00E+00 NA

2 1.20E-02 70.7 0.27 0 0 0 1.04E-03

79 2 162.8 2183 9.4 1.1 -1.45 1.94E-02 -1.49E-04 0.59 5.39E+04 NA

2 1.20E-02 70.7 2.64 0.65 5.15 3.98E-03 5.29E-04 0.34 1.03E-03 105.7

79 3 163.4 2580 13.82 1.8 -2.9 2.03E-02 -2.12E-04 0.64 6.40E+04 NA

2 1.21E-02 70.7 3.67 1.15 7.07 3.95E-03 5.17E-04 0.4 1.03E-03 112.3

79 4 164.2 2971 18.84 2.86 -4.11 2.08E-02 -2.26E-04 0.64 7.40E+04 NA

2 1.21E-02 70.7 5.05 1.82 9.66 4.08E-03 5.31E-04 0.46 1.02E-03 113.1

79 5 165.2 3168 22.05 3.49 -5.26 2.13E-02 -2.53E-04 0.66 7.94E+04 NA

2 1.22E-02 70.8 5.79 2.3 11.15 4.09E-03 5.36E-04 0.49 1.02E-03 115.3

79 6 166 2972 19.19 2.84 -4 2.10E-02 -2.17E-04 0.66 7.48E+04 NA

2 1.22E-02 70.8 5.02 1.86 9.03 4.01E-03 4.90E-04 0.46 1.01E-03 113.9

79 7 167.3 2577 14.38 1.84 -3.25 2.07E-02 -2.33E-04 0.65 6.54E+04 NA

99

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 1.23E-02 70.8 3.76 1.2 6.78 3.97E-03 4.86E-04 0.4 1.00E-03 115.6

79 8 167.9 2183 9.98 1.12 -1.92 2.00E-02 -1.91E-04 0.62 5.56E+04 NA

2 1.24E-02 70.8 2.7 0.69 5.21 3.95E-03 5.19E-04 0.34 9.99E-04 110.2

79 9 168.5 0 0 0 0 0.00E+00 NA

2 1.24E-02 70.8 0.28 0 0 0 9.95E-04

80 1 168.5 0 0 0 0 0.00E+00 NA

2 1.24E-02 70.8 0.28 0 0 0 9.95E-04

80 2 169.3 2181 10.05 1.13 -1.24 2.00E-02 -1.23E-04 0.62 5.60E+04 NA

2 1.25E-02 70.8 2.72 0.7 5.36 3.96E-03 5.30E-04 0.34 9.91E-04 103

80 3 170.1 2578 14.83 1.88 -3.46 2.10E-02 -2.44E-04 0.66 6.65E+04 NA

2 1.26E-02 70.8 3.83 1.25 7.83 3.97E-03 5.52E-04 0.4 9.86E-04 113.8

80 4 171.4 2576 14.92 1.89 -3.7 2.10E-02 -2.59E-04 0.67 6.70E+04 NA

2 1.26E-02 70.9 3.84 1.26 8.21 3.96E-03 5.75E-04 0.4 9.79E-04 114.3

80 5 172.1 2974 20.14 2.95 -4.41 2.12E-02 -2.31E-04 0.67 7.76E+04 NA

2 1.27E-02 70.9 5.21 1.97 10.67 4.01E-03 5.58E-04 0.46 9.75E-04 112.5

80 6 172.7 3170 23.06 3.62 -5.37 2.13E-02 -2.46E-04 0.66 8.31E+04 NA

2 1.27E-02 70.9 6 2.41 12.14 4.05E-03 5.57E-04 0.49 9.71E-04 113.9

80 7 173.3 2974 20.18 2.95 -4.9 2.11E-02 -2.55E-04 0.67 7.82E+04 NA

2 1.28E-02 70.9 5.21 1.97 10.98 3.98E-03 5.70E-04 0.46 9.68E-04 114.1

80 8 173.9 2576 15.07 1.91 -3.73 2.09E-02 -2.57E-04 0.66 6.80E+04 NA

2 1.28E-02 70.9 3.89 1.27 7.73 3.95E-03 5.33E-04 0.4 9.65E-04 115.8

80 9 174.5 2185 10.42 1.16 -2.16 2.00E-02 -2.06E-04 0.63 5.79E+04 NA

2 1.29E-02 70.9 2.79 0.73 5.84 3.93E-03 5.58E-04 0.34 9.62E-04 110.3

80 10 175.2 0 0 0 0 0.00E+00 NA

2 1.29E-02 70.9 0.28 0 0 0 9.58E-04

81 1 175.2 0 0 0 0 0.00E+00 NA

2 1.29E-02 70.9 0.28 0 0 0 9.58E-04

81 2 175.7 2183 10.5 1.18 -1.75 2.01E-02 -1.66E-04 0.62 5.82E+04 NA

2 1.30E-02 70.9 2.83 0.73 5.34 3.97E-03 5.08E-04 0.34 9.55E-04 108.1

81 3 176.3 2579 15.19 1.95 -3.04 2.08E-02 -2.06E-04 0.65 6.90E+04 NA

2 1.30E-02 70.9 3.97 1.27 7.27 3.96E-03 4.94E-04 0.4 9.52E-04 112.7

100

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

81 4 176.9 2976 20.36 3.07 -4.56 2.08E-02 -2.32E-04 0.64 7.99E+04 NA

2 1.31E-02 70.9 5.42 1.97 9.95 4.05E-03 5.06E-04 0.46 9.48E-04 114.6

81 5 177.8 3168 23.68 3.72 -6.13 2.13E-02 -2.74E-04 0.66 8.54E+04 NA

2 1.31E-02 70.9 6.17 2.47 11.74 4.05E-03 5.24E-04 0.49 9.44E-04 117.6

81 6 178.4 3168 23.81 3.76 -5.41 2.13E-02 -2.41E-04 0.66 8.57E+04 NA

2 1.32E-02 71 6.23 2.49 11.42 4.08E-03 5.08E-04 0.49 9.41E-04 115.4

81 7 179.1 2970 20.64 3.05 -4.06 2.09E-02 -2.05E-04 0.66 8.07E+04 NA

2 1.32E-02 71 5.4 2 10.04 4.00E-03 5.06E-04 0.46 9.37E-04 112

81 8 179.6 2574 15.4 1.97 -3.42 2.07E-02 -2.29E-04 0.65 7.02E+04 NA

2 1.33E-02 70.9 4.02 1.29 7.38 3.96E-03 4.94E-04 0.4 9.34E-04 114.9

81 9 180.3 2183 10.71 1.2 -1.45 2.00E-02 -1.34E-04 0.62 5.97E+04 NA

2 1.33E-02 71 2.88 0.75 5.02 3.93E-03 4.65E-04 0.34 9.31E-04 106.1

81 10 180.8 0 0 0 0 0.00E+00 NA

2 1.33E-02 71 0.28 0 0 0 9.28E-04

82 1 180.8 0 0 0 0 0.00E+00 NA

2 1.33E-02 71 0.28 0 0 0 9.28E-04

82 2 181.5 2187 10.85 1.22 -2.03 2.00E-02 -1.86E-04 0.62 6.02E+04 NA

2 1.34E-02 71 2.94 0.76 5.52 3.97E-03 5.07E-04 0.34 9.25E-04 110.1

82 3 182.2 2578 15.71 2 -3.28 2.08E-02 -2.16E-04 0.66 7.12E+04 NA

2 1.34E-02 71 4.08 1.32 7.87 3.95E-03 5.18E-04 0.4 9.21E-04 112.6

82 4 182.7 2976 21.17 3.15 -4.79 2.10E-02 -2.36E-04 0.65 8.25E+04 NA

2 1.35E-02 71 5.56 2.06 10.49 4.03E-03 5.16E-04 0.46 9.18E-04 114.6

82 5 183.5 3169 24.93 3.88 -6.65 2.17E-02 -2.87E-04 0.68 8.82E+04 NA

2 1.35E-02 71.1 6.44 2.63 12.69 4.09E-03 5.48E-04 0.49 9.14E-04 117.6

82 6 184.3 2965 21.62 3.14 -5.02 2.14E-02 -2.47E-04 0.67 8.29E+04 NA

2 1.36E-02 71.1 5.56 2.12 11.24 4.02E-03 5.53E-04 0.46 9.11E-04 114.1

82 7 184.9 2577 16.02 2.03 -3.39 2.09E-02 -2.20E-04 0.66 7.23E+04 NA

2 1.36E-02 71 4.14 1.35 8.07 3.95E-03 5.24E-04 0.4 9.08E-04 112.8

82 8 185.4 2183 11.17 1.24 -2.39 2.03E-02 -2.16E-04 0.63 6.14E+04 NA

2 1.37E-02 71.1 2.98 0.78 5.39 3.95E-03 4.86E-04 0.34 9.05E-04 113.9

82 9 186 0 0 0 0 0.00E+00 NA

2 1.37E-02 71.1 0.27 0 0 0 9.03E-04

101

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

83 1 186 0 0 0 0 0.00E+00 NA

2 1.37E-02 71.1 0.27 0 0 0 9.03E-04

83 2 186.6 2179 11.24 1.25 -1.73 2.03E-02 -1.56E-04 0.63 6.17E+04 NA

2 1.38E-02 71.1 3 0.79 5.57 3.97E-03 5.01E-04 0.34 9.00E-04 107.3

83 3 187.3 2579 16.33 2.06 -3.47 2.10E-02 -2.22E-04 0.67 7.33E+04 NA

2 1.38E-02 71.1 4.2 1.38 8.56 3.95E-03 5.47E-04 0.4 8.96E-04 112.1

83 4 188.2 2972 22.35 3.23 -6.19 2.16E-02 -2.97E-04 0.68 8.48E+04 NA

2 1.39E-02 71.1 5.7 2.2 13.51 4.02E-03 6.48E-04 0.46 8.92E-04 114.6

83 5 189.1 2578 16.58 2.11 -3.39 2.11E-02 -2.15E-04 0.67 7.39E+04 NA

2 1.39E-02 71.1 4.3 1.4 8.47 4.01E-03 5.37E-04 0.4 8.87E-04 111.8

83 6 190.2 2183 11.46 1.27 -1.5 2.03E-02 -1.32E-04 0.64 6.30E+04 NA

2 1.40E-02 71.1 3.04 0.8 5.56 3.94E-03 4.89E-04 0.34 8.82E-04 105.1

83 7 190.8 0 0 0 0 0.00E+00 NA

2 1.41E-02 71.1 0.27 0 0 0 8.80E-04

84 1 190.8 0 0 0 0 0.00E+00 NA

2 1.41E-02 71.1 0.27 0 0 0 8.80E-04

84 2 191.5 2182 11.61 1.29 -2.34 2.04E-02 -2.05E-04 0.64 6.34E+04 NA

2 1.41E-02 71.1 3.09 0.82 5.78 3.98E-03 5.05E-04 0.34 8.77E-04 112.1

84 3 192.1 2580 16.82 2.12 -4.08 2.11E-02 -2.54E-04 0.67 7.52E+04 NA

2 1.42E-02 71.1 4.31 1.42 9.37 3.96E-03 5.84E-04 0.4 8.74E-04 113.5

84 4 192.6 2973 22.79 3.32 -4.54 2.15E-02 -2.13E-04 0.67 8.69E+04 NA

2 1.42E-02 71.1 5.86 2.24 12.31 4.04E-03 5.76E-04 0.46 8.71E-04 110.3

84 5 193.2 2578 17.09 2.14 -4.14 2.13E-02 -2.57E-04 0.68 7.56E+04 NA

2 1.43E-02 71.1 4.36 1.45 8.79 3.98E-03 5.45E-04 0.4 8.69E-04 115.2

84 6 193.9 2182 11.68 1.29 -1.61 2.03E-02 -1.39E-04 0.63 6.42E+04 NA

2 1.43E-02 71.2 3.12 0.82 6.45 3.96E-03 5.57E-04 0.34 8.66E-04 104

84 7 194.5 0 0 0 0 0.00E+00 NA

2 1.43E-02 71.1 0.27 0 0 0 8.63E-04

85 1 196.2 0 0 0 0 0.00E+00 NA

2 1.45E-02 71.2 0.27 0 0 0 8.56E-04

102

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

85 2 221.3 1246 3.63 0.29 -0.3 1.70E-02 -6.86E-05 0.46 4.18E+04 NA

2 1.63E-02 71.3 1.23 0.13 1.97 4.21E-03 4.57E-04 0.19 7.58E-04 98.5

85 3 240.9 1245 3.95 0.31 0.03 1.70E-02 5.91E-06 0.47 4.55E+04 NA

2 1.77E-02 71.5 1.3 0.14 2.25 4.09E-03 4.79E-04 0.19 6.97E-04 89.3

85 4 260.5 1245 4.45 0.33 0.19 1.77E-02 3.79E-05 0.5 4.91E+04 NA

2 1.92E-02 72.1 1.4 0.17 2.19 4.08E-03 4.33E-04 0.19 6.45E-04 85

85 5 280.5 1245 4.93 0.36 0.17 1.82E-02 3.19E-05 0.53 5.28E+04 NA

2 2.06E-02 72.8 1.5 0.19 2.24 4.05E-03 4.11E-04 0.19 6.01E-04 85.6

85 6 297.9 1245 5.22 0.38 0.38 1.82E-02 6.54E-05 0.53 5.60E+04 NA

2 2.19E-02 73.3 1.59 0.2 3 4.04E-03 5.20E-04 0.19 5.66E-04 82.8

85 7 315.3 1245 5.46 0.39 0.73 1.80E-02 1.19E-04 0.52 5.92E+04 NA

2 2.31E-02 73.8 1.66 0.21 2.16 4.00E-03 3.54E-04 0.19 5.36E-04 71.4

85 8 334 1245 5.92 0.42 0.93 1.84E-02 1.44E-04 0.54 6.26E+04 NA

2 2.45E-02 74.3 1.76 0.23 2.25 4.00E-03 3.48E-04 0.19 5.06E-04 67.5

85 9 351.9 1245 6.3 0.44 0.83 1.86E-02 1.22E-04 0.55 6.58E+04 NA

2 2.58E-02 74.8 1.84 0.24 2.83 3.99E-03 4.16E-04 0.19 4.81E-04 73.7

85 10 368.2 1245 6.55 0.45 0.92 1.85E-02 1.30E-04 0.55 6.88E+04 NA

2 2.69E-02 75.2 1.91 0.25 2.68 3.94E-03 3.77E-04 0.19 4.61E-04 71

85 11 385.6 1245 7.04 0.47 0.97 1.90E-02 1.30E-04 0.58 7.20E+04 NA

2 2.82E-02 75.7 2 0.27 3.05 3.95E-03 4.09E-04 0.19 4.41E-04 72.4

85 12 406.7 1245 7.42 0.5 0.63 1.91E-02 8.02E-05 0.58 7.57E+04 NA

2 2.97E-02 76.3 2.09 0.29 3.19 3.93E-03 4.07E-04 0.19 4.18E-04 78.8

85 13 428.9 1245 7.94 0.52 1.11 1.94E-02 1.34E-04 0.6 7.97E+04 NA

2 3.13E-02 77 2.19 0.31 3.48 3.90E-03 4.22E-04 0.19 3.98E-04 72.4

85 14 446.5 1245 8.34 0.54 0.72 1.96E-02 8.40E-05 0.6 8.29E+04 NA

2 3.25E-02 77.5 2.29 0.33 3.89 3.93E-03 4.53E-04 0.19 3.82E-04 79.5

85 15 462 1245 8.59 0.55 1.43 1.95E-02 1.61E-04 0.61 8.57E+04 NA

2 3.36E-02 77.8 2.34 0.34 4.52 3.88E-03 5.10E-04 0.19 3.70E-04 72.5

85 16 481.2 1245 8.99 0.58 1.03 1.96E-02 1.12E-04 0.61 8.91E+04 NA

2 3.50E-02 78.3 2.45 0.35 3.74 3.91E-03 4.06E-04 0.19 3.56E-04 74.6

85 17 500.3 1245 9.22 0.6 0.85 1.93E-02 8.88E-05 0.6 9.25E+04 NA

2 3.64E-02 78.7 2.53 0.36 4.27 3.88E-03 4.46E-04 0.19 3.43E-04 78.7

85 18 516.4 1245 9.57 0.62 0.44 1.95E-02 4.42E-05 0.6 9.53E+04 NA 103

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 3.75E-02 79.1 2.63 0.38 4.03 3.91E-03 4.07E-04 0.19 3.32E-04 83.8

85 19 535.8 1244 10.11 0.64 0.9 1.98E-02 8.75E-05 0.62 9.88E+04 NA

2 3.89E-02 79.6 2.72 0.4 4.44 3.91E-03 4.33E-04 0.19 3.21E-04 78.6

85 20 554.7 1244 10.45 0.66 0.38 1.98E-02 3.63E-05 0.62 1.02E+05 NA

2 4.02E-02 80 2.8 0.41 4.49 3.88E-03 4.23E-04 0.19 3.10E-04 85.1

85 21 571.8 1244 10.79 0.68 0.49 1.99E-02 4.52E-05 0.63 1.05E+05 NA

2 4.14E-02 80.4 2.88 0.43 4.61 3.87E-03 4.22E-04 0.19 3.01E-04 83.9

85 22 589.9 1244 11.26 0.7 0.33 2.01E-02 2.97E-05 0.64 1.08E+05 NA

2 4.27E-02 80.7 2.97 0.45 5.38 3.89E-03 4.78E-04 0.19 2.92E-04 86.5

85 23 606.5 1244 11.7 0.73 -0.14 2.03E-02 -1.24E-05 0.65 1.11E+05 NA

2 4.39E-02 81 3.06 0.47 5.49 3.90E-03 4.74E-04 0.19 2.85E-04 91.5

85 24 622.1 1244 11.85 0.74 0.02 2.01E-02 2.01E-06 0.64 1.14E+05 NA

2 4.50E-02 81.3 3.1 0.47 6.12 3.85E-03 5.16E-04 0.19 2.78E-04 89.8

85 25 640.4 1244 12.38 0.76 0.17 2.04E-02 1.41E-05 0.66 1.17E+05 NA

2 4.63E-02 81.6 3.2 0.5 6.36 3.86E-03 5.21E-04 0.19 2.70E-04 88.5

85 26 658 1244 12.73 0.78 -0.02 2.04E-02 -1.34E-06 0.66 1.20E+05 NA

2 4.76E-02 81.9 3.28 0.51 6.94 3.85E-03 5.54E-04 0.19 2.63E-04 90.1

85 27 675.2 1244 13.07 0.8 -0.06 2.05E-02 -4.93E-06 0.66 1.23E+05 NA

2 4.88E-02 82.2 3.36 0.53 6.39 3.85E-03 4.98E-04 0.19 2.57E-04 90.6

85 28 693.2 1244 13.47 0.82 -0.64 2.06E-02 -4.89E-05 0.66 1.27E+05 NA

2 5.01E-02 82.5 3.45 0.54 7.03 3.85E-03 5.33E-04 0.19 2.50E-04 95.2

85 29 723 1244 14.14 0.85 -1.17 2.07E-02 -8.50E-05 0.67 1.32E+05 NA

2 5.22E-02 82.9 3.6 0.57 7 3.86E-03 5.10E-04 0.19 2.40E-04 99.5

85 30 741.3 1244 14.42 0.86 -0.49 2.06E-02 -3.47E-05 0.67 1.35E+05 NA

2 5.35E-02 83.2 3.65 0.58 6.94 3.81E-03 4.93E-04 0.19 2.34E-04 94

85 31 754.1 1244 14.71 0.88 -1.24 2.07E-02 -8.68E-05 0.67 1.37E+05 NA

2 5.44E-02 83.3 3.72 0.59 7.82 3.82E-03 5.47E-04 0.19 2.30E-04 99

85 32 773.3 1243 15.06 0.9 -1.66 2.07E-02 -1.13E-04 0.67 1.41E+05 NA

2 5.57E-02 83.6 3.81 0.61 7.56 3.83E-03 5.16E-04 0.19 2.25E-04 102.3

85 33 786.9 1243 15.16 0.91 -0.75 2.04E-02 -5.05E-05 0.67 1.43E+05 NA

2 5.67E-02 83.7 3.85 0.61 7.85 3.80E-03 5.26E-04 0.19 2.21E-04 95.5

85 34 801 1243 15.64 0.93 -1.08 2.07E-02 -7.12E-05 0.68 1.46E+05 NA

2 5.77E-02 83.7 3.93 0.63 8.64 3.81E-03 5.69E-04 0.19 2.17E-04 97.1

104

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

85 35 817.9 1243 16.07 0.95 -2.3 2.09E-02 -1.48E-04 0.68 1.49E+05 NA

2 5.89E-02 83.9 4.02 0.65 9.33 3.82E-03 6.02E-04 0.19 2.13E-04 103.8

85 36 831.5 1243 16.39 0.97 -3.05 2.09E-02 -1.94E-04 0.68 1.51E+05 NA

2 5.99E-02 84 4.11 0.67 7.83 3.84E-03 4.97E-04 0.19 2.09E-04 111.3

85 37 844.1 1243 16.74 0.99 -3.19 2.11E-02 -1.99E-04 0.69 1.53E+05 NA

2 6.08E-02 84.1 4.17 0.68 8.26 3.84E-03 5.17E-04 0.19 2.06E-04 111.1

85 38 856.1 1243 16.92 0.99 -3.72 2.10E-02 -2.30E-04 0.7 1.56E+05 NA

2 6.16E-02 84.1 4.17 0.69 9.71 3.78E-03 5.99E-04 0.19 2.03E-04 111

85 39 867.6 1243 16.96 0.99 -2.45 2.08E-02 -1.49E-04 0.69 1.58E+05 NA

2 6.25E-02 84.2 4.2 0.69 8.61 3.76E-03 5.24E-04 0.19 2.01E-04 105.9

85 40 879.9 1243 17.35 1.01 -3.33 2.10E-02 -2.00E-04 0.7 1.60E+05 NA

2 6.33E-02 84.2 4.26 0.7 9.3 3.76E-03 5.58E-04 0.19 1.98E-04 109.7

85 41 892 1243 17.34 1.02 -2.62 2.07E-02 -1.56E-04 0.69 1.62E+05 NA

2 6.42E-02 84.2 4.31 0.7 8.08 3.75E-03 4.79E-04 0.19 1.95E-04 108

85 42 901.7 1243 17.73 1.03 -2.82 2.09E-02 -1.66E-04 0.7 1.64E+05 NA

2 6.49E-02 84.2 4.37 0.72 8.48 3.76E-03 4.97E-04 0.19 1.93E-04 108.4

85 43 909.9 1243 17.71 1.04 -2.56 2.07E-02 -1.49E-04 0.69 1.65E+05 NA

2 6.55E-02 84.1 4.38 0.71 9.84 3.74E-03 5.72E-04 0.19 1.91E-04 104.6

85 44 925 1243 18.34 1.05 -3.13 2.11E-02 -1.79E-04 0.71 1.68E+05 NA

2 6.66E-02 84 4.44 0.75 9.69 3.73E-03 5.53E-04 0.19 1.88E-04 107.9

85 45 933.7 1243 18.37 1.07 -3.92 2.09E-02 -2.22E-04 0.7 1.70E+05 NA

2 6.72E-02 83.9 4.51 0.75 8.88 3.75E-03 5.03E-04 0.19 1.86E-04 113.8

85 46 940.5 1243 18.54 1.07 -3.42 2.09E-02 -1.92E-04 0.7 1.71E+05 NA

2 6.77E-02 83.9 4.51 0.75 10.13 3.73E-03 5.69E-04 0.19 1.85E-04 108.7

85 47 947.6 1243 18.62 1.07 -3.49 2.09E-02 -1.94E-04 0.7 1.72E+05 NA

2 6.82E-02 83.8 4.54 0.75 9.55 3.72E-03 5.33E-04 0.19 1.84E-04 110

85 48 953.7 1242 19.28 1.1 -4.76 2.15E-02 -2.64E-04 0.72 1.73E+05 NA

2 6.87E-02 83.8 4.64 0.79 9.54 3.78E-03 5.29E-04 0.19 1.82E-04 116.5

85 49 960 1242 18.97 1.09 -4.15 2.10E-02 -2.28E-04 0.71 1.75E+05 NA

2 6.92E-02 83.7 4.61 0.77 9.67 3.73E-03 5.32E-04 0.19 1.81E-04 113.2

85 50 966.6 1243 19.26 1.1 -3.49 2.12E-02 -1.91E-04 0.71 1.76E+05 NA

2 6.96E-02 83.6 4.66 0.79 10.07 3.74E-03 5.50E-04 0.19 1.80E-04 109.1

85 51 972.7 1243 19.34 1.11 -4.56 2.11E-02 -2.47E-04 0.71 1.77E+05 NA 105

run point p [mbar] RPM [~] T [lb] P [hp] Mx [in-lb] CT [~] CMx [~] FM [~] Re.75 [~] V [ft/s]

n [~] rho [lb/ft3] T [F] Q [ft-lb] Pi [hp] My [in-lb] CP [~] CMy [~] Mtip [~] nu [ft

2/s] phi [deg]

2 7.01E-02 83.5 4.68 0.79 9.78 3.74E-03 5.31E-04 0.19 1.79E-04 115

85 52 977.1 1242 19.41 1.12 -3.14 2.11E-02 -1.70E-04 0.71 1.78E+05 NA

2 7.04E-02 83.4 4.72 0.79 10.37 3.75E-03 5.61E-04 0.19 1.78E-04 106.8

85 53 981.8 1243 19.3 1.12 -5.14 2.09E-02 -2.76E-04 0.7 1.79E+05 NA

2 7.08E-02 83.3 4.72 0.78 10.98 3.74E-03 5.91E-04 0.19 1.77E-04 115.1

85 54 987.1 1242 19.71 1.13 -4.3 2.12E-02 -2.30E-04 0.71 1.80E+05 NA

2 7.12E-02 83.2 4.77 0.8 11.51 3.76E-03 6.16E-04 0.19 1.76E-04 110.5

85 55 991 1242 19.61 1.13 -3.81 2.10E-02 -2.03E-04 0.7 1.81E+05 NA

2 7.15E-02 83.1 4.8 0.8 10.65 3.76E-03 5.67E-04 0.19 1.75E-04 109.7

85 56 995.3 1242 19.73 1.14 -4.42 2.10E-02 -2.35E-04 0.7 1.81E+05 NA

2 7.18E-02 83 4.82 0.8 10.88 3.76E-03 5.77E-04 0.19 1.74E-04 112.1

85 57 1004.9 1242 19.9 1.15 -4.55 2.10E-02 -2.39E-04 0.7 1.83E+05 NA

2 7.25E-02 82.7 4.85 0.81 11.31 3.75E-03 5.94E-04 0.19 1.72E-04 111.9

85 58 1007.8 1242 19.93 1.15 -5.04 2.10E-02 -2.63E-04 0.7 1.84E+05 NA

2 7.28E-02 82.4 4.88 0.81 11.6 3.75E-03 6.07E-04 0.19 1.72E-04 113.5

85 59 1014.4 0 0 0 0 0.00E+00 NA

2 7.33E-02 82 0.4 0 0 0 1.70E-04

86 1 1014.8 0 0 0 0 0.00E+00 NA

2 7.34E-02 81.4 0.36 0 0 0 1.70E-04

86 2 1014.7 500 2.61 0.08 0 1.68E-02 -1.06E-06 0.46 7.49E+04 4.1

2 7.34E-02 81.3 0.87 0.04 1.23 4.08E-03 3.94E-04 0.08 1.70E-04 90.2

86 3 1014.7 998 12.49 0.62 -2.41 2.02E-02 -1.94E-04 0.65 1.50E+05 9.2

2 7.35E-02 81.1 3.24 0.4 7.11 3.83E-03 5.71E-04 0.15 1.70E-04 108.7

86 4 1014.7 1240 20.2 1.18 -5.66 2.11E-02 -2.95E-04 0.7 1.86E+05 11.7

2 7.35E-02 81 4.99 0.82 10.65 3.82E-03 5.54E-04 0.19 1.70E-04 118

86 5 1014.7 999 12.65 0.61 -2 2.04E-02 -1.60E-04 0.67 1.50E+05 9.2

2 7.35E-02 80.8 3.22 0.41 6.66 3.79E-03 5.33E-04 0.15 1.70E-04 106.7

86 6 1014.6 500 2.67 0.08 -0.13 1.72E-02 -4.06E-05 0.5 7.50E+04 4.2

2 7.35E-02 80.6 0.84 0.04 1.2 3.93E-03 3.82E-04 0.08 1.70E-04 96.1

86 7 1014.6 0 0 0 0 0.00E+00 NA

2 7.35E-02 80.5 0.49 0 0 0 1.70E-04

106


Recommended