text: where 
  
  VP= maneuver speed 
  
  V,= stall speed 
  
  n limit = limit  load factor 
  
  Of course, the stall speed and limit load factor 
  must be appropriate for 
  the airplane gross 
  weight. One notable fact is that this speed, 
  once properly computed, remains a constant 
  value if no significant change takes place in 
  the spanwise weight distribution. 
  The ma- 
  neuver speed of the subject aircraft of figure 
  5.4. would be 
  
  Aileron rever& is a phenomenon particular 
  to high speed flight. When in flight at very 
  high dynamic pressures, the wing 
  torsional 
  deflections which occur with aileron deflection 
  are considerable and cause noticeable change 
  in aileron effectiveness. The deflection of an 
  aileron on a rigid wing creates a change in lift 
  and produces a rolling moment. 
  In addition 
  the deflection of the control surface creates a 
  twisting moment on the wing. When the 
  actual elastic wing is subject to this condition 
  at high dynamic pressures, the twisting mo- 
  ment produces measurable twisting deforma- 
  tions which affect the rolling performance of 
  the aircraft. Figure 5.5 illustrates this process 
  and the effect of airspeed on aileron effective- 
  ness. At some high dynamic pressure, the 