NAVWEPS 00-801-80 
AIRPLANE PERFORMANCE 
A 
TURN 
RADIUS 
F: 
A-- I t 
VELOCITY, KNOTS (TAS) 
EFFECT OF AERODYNAMIC AND 
STRUCTURAL LIMIT ON TURNING 
PERFORMANCE 
ABSOLUTE MINIMUM 
L 
TURN 
RADIUS 
F: 
CONSTANT ALTITUDE TURNING 
PERFORMANCE 
I 
,-INCREASING 
BANK ANGLE 
THRUST OR 
t 
VELOCITY, KNOTS (TAS) 
figure 2.30. Maneuvering Performance 
181