text: Spinrecovety..; 
  Slipstream rotatmn. ................................................ 
  Cross wind takeoff and landing. 
  Asymmetrical power. ............................................... 
  
  ................................................... 
  
  LATERAL  STABILITY AND CONTROL 
  
  ........................................... 
  LATERAL STABILITY, 
  
  Definlttons  ........................................................... 
  
  CONTRIBUTION OF THE AIRPLANE COMPONENTS. 
  
  295 
  298 
  Wing.........~.........~ 
  Fuselage and wmg powton, ................................................................................... 
  298 
  298 
  Sweepback ......................................................... 
  298 
  Vertical tail. ........................................................ 
  
  LATERAL DYNAMIC EFFECTS, ................................ 
  299 
  
  Directional divergence 
  Spiral divergence 
  Dutch roll 
  
  CONTROL IN ROLL .............................................. 
  Rolhsg motmn of an airplane. ...................................... 
  Roliing performance, .............................................. 
  Critical requirements. .............................................. 
  300 
  300 
  301 
  305 
  
  . 
  
  MISCELLANEOUS  STABILITY PROBLEMS 
  
  .........................  305 
  LANDING GEAR CONFIGURATIONS 
  
  Tail wheel type 
  Tricyde 
  type 
  Bicycle type 
  
  SPINS AND PROBLEMS OF SPIN RECOVERY ................ 
  307 
  
  Principal prospin moments 
  Fundamental principle of recovery 
  Effect of configuration 