Test 10 Questions ATPL - Airline Transport Pilot license - Principles of Flight, no time limit

1 - Which combination of speeds is applicable for structural strength in gust (clean configuration)?
2 - With increasing angle of attack, the stagnation point will move (I) ...and the point of lowest pressure will move (II) ...Respectively (I) and (II) are:
3 - Given two identical aeroplanes with wing mounted engines, one fitted with jet engines and the other with counter rotating propellers, what happens following an engine failure?
4 - The formula for the Mach Number is: (a= speed of sound)
5 - On a un-swept wing, when the aerofoil is accelerated from subsonic to supersonic speeds, the aerodynamic centre:
6 - For a fixed-pitch propeller in flight at a given TAS, the blade angle of attack will:
7 - The effect of a ventral fin on the static stability of an aeroplane is as follows: (1=longitudinal, 2=lateral, 3=directional)
8 - Rotation around the normal axis is called:
9 - Assuming no compressibility effects, induced drag at constant IAS is affected by:
10 - The angle of attack of a wing profile is defined as the angle between: