'Flutter' may be caused by:4
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What is the limit load factor of a large transport aeroplane?4
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Which combination of speeds is applicable for structural strength in gust (clean configuration)?4
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The angle of attack for a propeller blade is the angle between the blade chord line and the:4
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If in a two-dimensional incompressible and subsonic flow, the streamlines converge the static pressure in the flow will:4
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The Mean Aerodynamic Chord (MAC) for a given wing of any planform is4
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The point, where the single resultant aerodynamic force acts on an aerofoil, is called:4
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The critical angle of attack:4
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If flaps are deployed at constant IAS in straight and level flight, the magnitude of tip vortices will eventually: (flap span less than wing span)4
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Which one of the following statements about the lift-to-drag ratio in straight and level flight is correct?4
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