Chapter 2 Air and Air Flow

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    Air and Airflow

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    Air Resistance or DRAG

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    Effect of Streamlining

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    Air Resistance : Drag in aviation;

    Reduce as much as possible.

    Drag : Is due to FOR !pressure"

    and #$I% !surface"

    FOR : In front high pressure!Flat &late" !above normal"

    Reduced pressure

    !below normal" behind.Flow bifurcates in front'

    A stagnation point of

    highest pressure and

    no movement.

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    #treamlines : (ines showing the

    direction of flow of afluid at an) particular

    moment.

     #ucceeding molecules

    follow the same path.

    #treamlined #hape : inimum

    resistance'Fineness Ratio of * to +'

    a,imum thic-ness at

    about /* rd distance

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    #-in Friction : Due to viscosit)'

    Air at surface is

    brought to almoststand still.

      Gradual increase tillfree air speed.

      Increases with

    increase in speed

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    0oundar) (a)er : (a)er in which this

    change in speed occurs

      1hic-ness' more in turbulent la)er 

    (aminar Flow : One molecule follows

    another 

    1urbulent Flow : 2apha3ard' more energ)'

    1ransition &oint : 4here flow changes

    from laminar to turbulent.

    oves forward with

    increase in speed

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    0ernoulli5s : & 6 78 6 g3 9 onstant

    4here & is pressure' = is densit)'

    7 is velocit)' g is gravit) constant

    and 3 is change in height

    If change in height is negligible'

    g3 can be ignored.

    1hen & 6 ?=78 9 onstant

    & is #tatic and ?=78 is D)namic pressure

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    #tagnation pressure 9

    #tatic pressure 6

    D)namic pressure

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    Resistance : #hape of the bod)

    Depends on Frontal area of the bod)

      #

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    R(A1IO%#2I& 014%

    AIR#&D#

    • Indicated Airspeed !IA#". ASI (Pressure

    Gauge)

    • 1rue Airspeed !1A#". Corrected for

    Density error as well.

    • Ground #peed !G#". TAS corrected for

    local winds.