81-02. High Speed Aerodynamics
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1. When an aeroplane accelerates from subsonic to supersonic speed, the Aerodynamic Centre:
2. The speed of sound is affected by the:
3. Vortex generators on the upper side of the wing surface will:
4. Compared with an oblique shock wave at the same Mach number a normal shock wave has a:
5. Critical Mach number is the: