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

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
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
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

This note was uploaded on 05/17/2011 for the course PHY 2049 taught by Professor Any during the Spring '08 term at University of Florida.

Ask a homework question - tutors are online