Assuming an initial condition in straight and level flight with CL = 1. What will be the new value of CL after the value of the speed has doubled?4
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Which type of stall has the largest associated angle of attack?4
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After the transition point between the laminar and turbulent boundary layer4
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The wing of an aeroplane will never stall at low subsonic speeds as long as....4
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An aeroplane has a stall speed of 100 kt at a mass of 1000 kg. If the mass is increased to 2000 kg, the new value of the stall speed will be:4
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A slotted flap will increase the CLmax by:4
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During the retraction 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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One important advantage the turbulent boundary layer has over the laminar layer is that:4
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Assuming ISA conditions, which statement with respect to the climb is correct ?4
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When the Mach number is slowly increased in straight and level flight the first shockwaves will occur:4
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