ch06-p076 - 1 76 We use Eq 6-14 D = 2 CAv 2 where is the...

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76. We use Eq. 6-14, DC A v = 1 2 2 ρ , where is the air density, A is the cross-sectional area of the missile, v is the speed of the missile, and C is the drag coefficient. The area is given by
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