draveon556 draveon556

27-02-2024
Physics

contestada

An aircraft with a drag coefficient of 0.95 and a frontal area of 10m² is traveling at a Mach number of 0.7 in air with a static pressure of 101 kPa. Calculate the drag produced by this aircraft.

a. 665 N
b. 6650 N
c. 950 N
d. 9500 N

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