NAVWWS 00-8OT-80 
BASIC AERODYNAMICS 
.#a, GANK~ANGLE, DEGREES 
EFFECT OF c LMAX 
ONSTALL SPEED 
250 
200 
ANT 
150 % 
100 
50 
IO 20 30 40 50 
PERCENTDECREASE 
IN STALL SPEED 
Figure 7.76. Flight at High Liff Conditions 
38 
Revised Jarwary 1965