POD used as a filtering method

Post on 18-Jan-2016

23 views 0 download

description

Decompose the flow, and preserve the highest energy levels (Here upper 10%). Calculated Instantaneous velocity vectors. Subtract the Mean image. Raw Images. POD used as a filtering method. Example: Poorly seeded Helium Jet. Holes in gappy dataset - PowerPoint PPT Presentation

transcript

Slide 1 Den Haag September 2007

POD used as a filtering methodExample: Poorly seeded Helium Jet

Raw ImagesSubtract the Mean image

Calculated Instantaneous

velocity vectors

Decompose the flow, and preserve the highest energy levels (Here

upper 10%)

Slide 2 Den Haag September 2007

POD as filtering• Holes in gappy dataset

• Poorly seeded TR measurements often have that

VectorsImage POD Projection (90% of energy)

Slide 3 Den Haag September 2007

POD as filtering• Example – a jet where the surrounding air has not been seeded

Slide 4 Den Haag September 2007

EndoscopesSetup for 3D PIV

Two different endoscopes:

-Normal end

-45 slanted end

Slide 5 Den Haag September 2007

Endoscopic light sheet optics

Slide 6 Den Haag September 2007

300

310

320

330

340

350

360

370

380

390

400

410

0.5 1 1.5

0.5

0.6

0.7

0.8

0.9

1

1.1

1.2

1.3

1.4

1.5

ResultsRotor - Position 1in-plane velocity

-50

-40

-30

-20

-10

0

10

20

30

40

50

0.5 1 1.5

0.5

0.6

0.7

0.8

0.9

1

1.1

1.2

1.3

1.4

1.5

Rotor - Position 1out-of--plane velocity

Rotor-Position 1Instantaneous Vortivcity

More details about the measurements in a transonic test turbine can be found in: Lang et al., "Stereoscopic particle image velocimetry in a transonic turbine stage", Experiments in Fluids 32, 2002, pp 700-709

Slide 7 Den Haag September 2007

• Slow, low-turbulentwater flow

• 60 µm polyamide particles

• 20W AR-Ion laser w. scanning mirror

• NanoSense camera

• Frame rate ~100 Hz

• Measuring distance 3.7m(1.2 m in water)

• Measuring area820 x 1000 mm

I.e. almost 1 m2 !!!

Large area TR-PIV

Slide 8 Den Haag September 2007

Understanding tip vortices in detailswith PIV measurements in water

x/b=6.80.2 nm

K. & C. Huenecke, Airbus

x/b=30.00.9 nm

x/b=63.02.0 nm

1962 CTA measurements in open air,waiting for the fly-by of the aircraft

Wingtip vortices, then and now

Slide 9 Den Haag September 2007

Laser housing on vertical traverse

1 - 6 m down

10 m laserumbilical

Power supplyon platformTowed

aircraftmodel

Cross section of HSVA tank

Submerged PIV for large towing tank

Slide 10 Den Haag September 2007

Vector Field Vorticity

Click on the picture

Slide 11 Den Haag September 2007

Trajectory of the Vortex Core

y-z

Slide 12 Den Haag September 2007

Vector Field and Velocity Magnitude

Click on the picture

Slide 13 Den Haag September 2007

Thank you!