NAVWEPS 00-807-80  STABILITY AND CONTROL  P,  RAl  ^,  r%“LL  O/SEC.  0  ,/  <EiECT  0  OF ADDED  POWER  BOOST  V. KNOTS  4  ROLL .lD  HELIX  ANGLE  pb  TT  -  V, KNOTS  A  AILERON  -----  DEFLECTlON  8,  V.KNOTS  SPEED CORRESPONDING  TO LIMIT OF PILOT EFFORT  TO MAINTAIN MAXIMUM  DEFLECTION  A  (3  z  3  is  1.0  0  c  5  ELASTIC WING  TWISTING  REVERSAL  Figure 4.30. Control in Roll  304 