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In transonic region the mach number affects the aerodynamic characteristics.

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In transonic region the mach number affects the aerodynamic characteristics.

(a) True

(b) False

I got this question in semester exam.

The above asked question is from Aircraft Force Systems topic in chapter Aircraft Force Systems and the Equations of Motion of Aircraft Performance

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The correct answer is (a) True

Explanation: In transonic region the mach number affects the aerodynamic characteristics. Transonic region is a region in which the mach number ranges from 0.8 to 1.2. It depends on the airspeed of the aircraft and temperature of surroundings.

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