EASA ATPL 081 Principles Of Flight Practice Questions - EASA ATPL Theory - Principles Of Flight (081) Exam

Dynamic pressure (q) is calculated using which expression, where rho is air density and V is true airspeed?

rho x V 1/2 x rho^2 x V rho x V^2 1/2 x rho x V^2

Correct Answer:

1/2 x rho x V^2

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