This preview shows page 1. Sign up to view the full content.
76. We use Eq. 614,
DC
A
v
=
1
2
2
ρ
, where
is the air density,
A
is the crosssectional
area of the missile,
v
is the speed of the missile, and
C
is the drag coefficient. The area is
given by
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.
 Spring '08
 Any
 Physics

Click to edit the document details