text: and it produces the minimum 
  turn radius 
  within aerodynamic and structural limitations. 
  At speeds less than the maneuver speed, the 
  load factor is not available aerodynami- 
  limit 
  turning performance is aerody- 
  cally and 
  namically 
  limited. At speeds greater than 
  and maximum 
  the maneuver speed, CL- 
  aerodynamic load factor are not available and 
  limited. 
  turning performance is structurally 
  load factor 
  When the stall speed and limit 
  are known for a particular configuration, the 
  maneuver speed is related by the following 
  expression: 
  
  where 
  
  V,=maneuver speed, knots 
  V.=stall speed, knots 
  n limit = limit load factor 