NAVWEPS OD-BOT-80 
APPLICATION OF AERODYNAMICS 
TO SPECIFIC PROBLEMS OF FLYING 
EFFECT OF STEEP TURNS ON THRUST REQ’D 
THRUST 
REO’D 
LBS. 
WING LEVEL FLIGHT 
VARloUS 
APPROACH PATHS 
TYPICAL LIFT n 
CURVES 
LIFT 
COEFFICIENT 
CL 
ANGLE OF ATTACK, a 
Figure 6.4. The Approach and Landing