NAVWEPS 00-801-80 
APPLICATION OF AERODYNAMICS 
TO SPECIFIC PROBLEMS OF FLYING 
+Y 
I 
l--J-@$!?e 
DRAG 
\ SIN 7 = - j WEIGHT 
LIFT-OR&G 
RATIO 
L4l 
i 
GLIDE RATIO * L/o 
r )M 
-CLEAN CONFIGURATION 
! 
A <LANDING CONFIGURATION 
LIFT COEFFICIENT, CL 
RATE OF 
DESCENT, 
FPM 
CLEAN CONFIGURATION 
POWER OFF 
VELOCITY, KNOTS 
Figure 6.6. Glide Performance 
370