What is the effect on induced drag of mass and speed changes? (all other factors of importance remaining constant)4
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When an aeroplane is flying at an airspeed which is 1.3 times its basic stalling speed, the coefficient of lift as a percentage of the maximum lift coefficient (CLmax) would be:4
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A jet aeroplane cruises buffet free at high constant altitude. Which type of stall can occur if this aeroplane decelerates during an inadvertent increase in load factor?4
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Given an initial condition in straight and level flight with a speed of 1.4 VS. The maximum bank angle attainable without stalling in a steady co-ordinated turn, whilst maintaining speed and altitude, is approximately:4
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Deploying a Fowler flap, the flap will:4
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The trailing edge flaps when extended:4
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A plain flap will increase CLmax by4
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Spoiler deflection causes:4
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The flight Mach number is 0.8 and the TAS is 400 kts. The speed of sound is:4
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The critical Mach Number of an aeroplane is the free stream Mach Number, which produces the first evidence of:4
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