One disadvantage of wing sweep is the stalling characteristics. At the stall:4
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An aeroplane has a stall speed of 100 KT at a load factor n = 1. In a turn with a load factor of n = 2, the stall speed is:4
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When flaps are extended in a straight and level flight at constant IAS, the lift coefficient will eventually:4
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Given the following aeroplane configurations:1. Clean wing2. Slats only extended3. Flaps only extendedPlace these configurations in order of stall angle of attack:4
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The use of a slot in the leading edge of the wing enables the aeroplane to fly at a slower speed because:4
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The formula for the Mach Number is: (a= speed of sound)4
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In the transonic range the aeroplane characteristics are strongly determined by:4
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When the air is passing through a shock wave the static temperature will4
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In the transonic range lift will decrease at the shock stall due to the4
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The speed range between high- and low speed buffet:4
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