Which one of the bodies in motion (all bodies have the same cross section area) will have lowest drag?4
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Which of the following statements about the spin is correct?4
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During an erect spin recovery:4
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Which combination of design features is known to be responsible for deep stall?4
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In a stationary subsonic streamline flow pattern, if the streamlines converge, in this part of the pattern, the static pressure (I) will ...and the velocity (II) will ...:4
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The angle between the airflow (relative wind) and the chord line of an aerofoil is:4
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The true airspeed (TAS) is:4
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What is the SI unit of measurement for power?4
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On an asymmetrical, single curve aerofoil, in subsonic airflow, at low angle of attack, when the angle of attack is increased, the centre of pressure will (assume a conventional transport aeroplane):4
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The frontal area of a body, placed in a certain airstream is increased by a factor 3. The shape will not alter. The aerodynamic drag will increase with a factor:4
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