An aeroplane has a stalling speed of 100 KT in a steady level flight. When the aeroplane is flying a level turn with a load factor of 1.5, the stalling speed is:4
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The lift formula is: (rho = density)4
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The angle of attack of a blade section is the angle between the chord line and the:4
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When a jet transport aeroplane takes off with the CG at the forward limit and the trimmable horizontal stabiliser (THS) is positioned at the maximum allowable nose up position for take- off:4
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Rotation around the normal axis is called:4
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A jet transport aeroplane exhibits pitch up when thrust is suddenly increased from an equilibrium condition, because the thrust line is below the:4
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For a fixed-pitch propeller in flight at a given TAS, the blade angle of attack will:4
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A "slat" is:4
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Assuming no compressibility effects, induced drag at constant IAS is affected by:4
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If the trailing edge flaps are lowered (fully extended), in order to maintain constant IAS and level flight:4
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