Brunei DCA CPL(A) Principles Of Flight Practice Questions - Brunei DCA CPL(A) Theoretical Knowledge - Principles Of Flight (Aeroplanes) Exam

How is dynamic pressure mathematically defined in subsonic aerodynamics?

q = 0.5 * rho * V^2 q = rho * V / 2 q = P_static + P_total q = 0.5 * P_static * V^2

Correct Answer:

q = 0.5 * rho * V^2

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