NAVWEPS 00-801-80  APPLICATION OF AERODYNAMICS  TO SPECIFIC PROBLEMS OF FLYING  +Y  I  l--J-@$!?e  DRAG  \  SIN 7 =  -  j  WEIGHT  LIFT-OR&G  RATIO  L4l  i  GLIDE RATIO * L/o  r  )M  -CLEAN  CONFIGURATION  !  A <LANDING  CONFIGURATION  LIFT COEFFICIENT, CL  RATE OF  DESCENT,  FPM  CLEAN CONFIGURATION  POWER OFF  VELOCITY, KNOTS  Figure 6.6. Glide Performance  370 