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djester555
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Homework Statement
Missile Calculate the drag force on a missile 48 cm in diameter cruising with a speed of 270 m/s at low altitude, where the density of air is 1.2 kg/m3. Assume C = 0.75.
Homework Equations
Fd = -1/2p(v^2)CA
The Attempt at a Solution
-1/2(1.2)(270^2)(0.75(0.48) = -15746.4 what am i doing wrong?