figure 2.30. Maneuvering Performance  181  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) 