text: sweep Angle (A): 
  
  O”................................. 
  w................................ 
  300. 
  450.......... 
  M)Q................................ 
  
  The reduction of the low speed maximum 
  lift coefficient (which is in addition to that 
  lost due to tip stall) has very important 
  If wing loading is 
  implications in design. 
  not reduced, stall speeds increase and sub- 
  sonic maneuverability decreases. On the 
  other hand, if wing loading is reduced, the 
  increase in wing surface area may reduce 
  the anticipated benefit of sweepback in the 
  transonic flight regime. Since the require- 
  ments of performance predominate, certain 
  increases of stall speeds, takeoff speeds, 