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 