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International Standard Atmosphere (ISA)

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    The most important single factor

    influencing learning is what the

    learner already knows. Ascertain this

    and teach him accordingly.DavidAusubel-Educational psychology: A cognitive approach, 1968.

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    Aerodynamics

    Physical quantities of a flowing gas

    Source of aerodynamic force-flow field

    Equation of state for perfect gas

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    STREAMLINES

    STREAMLINES REPRESENT A FLOW AND IS DEFINED AS

    IMAGINARY LINES ACROSS WHICH THERE IS NO FLOW.THE CLOSENESS OF STREAMLINES GIVE AN INDICATION

    OF FLOW SPEED

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    HARRIER INSTANTANEOUS STREAMLINES

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    WATER STREAMLINES ON F-16 MODEL

    http://www.aerolab.com/water.html

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    TYPES OF FLOWS: FRICTION VS. NO-FRICTION

    Viscous: Flows with friction

    All real flows are viscous

    Inviscid flow is a useful idealization

    By neglecting friction analysis of flow is usually much easier!

    Inviscid: Flows with no friction

    Flow very close to surface of airfoil is

    Influenced by friction and is viscous

    (boundary layer flow)

    Stall (separation) is a viscous phenomena

    Flow away from airfoil is not influenced

    by friction and is wholly inviscid

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    TYPES OF FLOWS:

    COMPRESSIBLE VS. INCOMPRESSIBLE

    Compressible: Density of fluid elements may change from point to

    point All real flows are compressible

    Important for gases (rarely important for liquids)

    Most important at high speeds

    Incompressible: Density of fluid elements is always constant

    General Rule of Thumb:

    If flow speed is less than about 100 m/s (or less than 225 MPH) flow can be considered incompressible

    or

    If flow is less than Mach 0.3, flow can be consideredincompressible

    Mach number, M: ratio of local velocity to local speed of

    sound, V/a

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    Flight velocities over the years

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    Flight altitudes over the years

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    The Standard Atmosphere

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    Solar Energy as Radiation

    Nearly 150 million kilometers separate the sun and earth, yet solar radiation drives earth's

    weather.

    E th' At h

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    Earth's Atmosphere

    99% of atmospheric gases, including water vapor, extend only 30 kilometer (km) above earth's

    surface.

    Most of our weather, however, occurs within the first 10 to 15 km.

    Thin Gaseous envelope

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    The Standard Atmosphere

    Dynamically changing system

    Need of standard atmosphere (P,T and )

    Flight test, Wind tunnel results and Aircraftperformance

    SAmean values of P,T and as a function of

    altitude

    Table of common ref

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    The Standard Atmosphere

    Altitude-Quantitative use Geometric altitude (hG)

    Absolute altitude (ha)

    Local gravitational acceleration (g)

    Sea level gravitational acceleration

    (go) Geopotential altitude (h)

    Pressure & Density

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    Pressure & Density

    The amount of force

    exerted Over an area

    of surface is called

    Air pressure!Air Density is

    The number of air

    Molecules in a given

    Space (volume)

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    Vertical Pressure Profile

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    Vertical Pressure Profile

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    Hydrostatic Equation

    Force balance on element

    of fluid

    Variation of Pr and Density

    with altitude

    dp = - *g*dhGdp = - *go*dh

    Geopotential altitude

    If the net upward pressure force on the slab is equal to the

    downward force of gravity on the slab, the atmosphere is said

    to be in hydrostatic balance.

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    Geopotential and Geometric Altitude

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    ?

    S

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    Summary

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    Standard Atmosphere

    The values of temperature, pressure and

    density are never constant in any given layerof the atmosphere .

    Requirement for a standard atmosphere for

    the comparison of aircraft performances,calibration of altimeters and other practicaluses.

    Standard Atmosphere (ISA) defined by the

    International Civil Aviation Organization(ICAO).

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    Standard Atmosphere

    The ISA assumes a mean sea level Temp of

    +15C, a pressure of 1013.25 mb (14.7 psi) and

    a density of 1.225 kg /m3.

    The temperature lapse rate is assumed to be

    uniform at the rate of 6.5K per kilometer up

    to the height of 11 km (36,090 ft) above which

    it remains constant at 216.66 K

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    The Hydrostatic Equation

    Air pressure at any height in the atmosphere is due to theforce per unit area exerted by the weight of all of the airlying above that height. Consequently, atmosphericpressure decreases with increasing height above theground.

    The net upward force acting on a thin horizontal slab of air,due to the decrease in atmospheric pressure with height, isgenerally very closely in balance with the downward forcedue to gravitational attraction that acts on the slab.

    If the net upward pressure force on the slab is equal to thedownward force of gravity on the slab, the atmosphere issaid to be in hydrostatic balance.


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