NAVWEPS 00-801-80 
BASIC AERODYNAMICS 
1.4 
1.2 
iL 
i 0.4 
0.2 
0 
0 .05 ;!O .!5 
DRAG COEFFICIENT, CD 
I.4 
I.2 
j 1.0 
^ 
5 
t 0.6 
ii 
kl $ 0.6 
t 
i 0.4 
0.2 
0 
DRAG COEFFICIENT, CD 
Figure 1.34. Airplane Parasite and Induced Drag