text: v.2 
  =(-) V*
  
  Thus, if the airplane is flying at twice the 
  stall speed and the angle of attack is increased 
  to obtain maximum 
  load 
  factor of four will result. At three times the 
  four 
  stall speed, nine “g’s” 
  times the stall speed, sixteen g’s result; five 
  times the stall speed, twenty-five g’s result; 
  etc. Therefore, any airplane which has high 
  speed performance may have the capability of 
  high maneuvering load factors. The airplane 
  is capable of flight speeds that are 
  which 
  
  lift, a maximum 
  
  would  result; 