The stall speed:4
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Vortex generators:4
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In order to maintain straight and level flight at a constant airspeed, whilst the flaps are being retracted, the angle of attack must be:4
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Deflection of leading edge flaps will:4
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During the extension of the flaps at a constant angle of attack the aeroplane starts to (all other factors of importance being constant)4
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During a climb at a constant IAS, the Mach Number:4
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The consequences of exceeding Mcrit in a swept-wing aeroplane may be: (assume no corrective devices, straight and level flight)4
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When comparing a rectangular wing and a swept back wing of the same wing area and wing loading, the swept back wing has the advantage of:4
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Just above the critical Mach number the first evidence of a shock wave will appear at the4
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High speed buffet is induced by4
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