1.4  1.2  iL  i  0.4  0.2  0  0  .05  ;!O  .!5  DRAG COEFFICIENT, CD  I.4  I.2  j  1.0  ^  5  t  0.6  ii  kl  $  0.6  t  i  0.4  0.2  0  DRAG COEFFICIENT, CD  Figure 1.34. Airplane Parasite and Induced Drag  NAVWEPS 00-801-80  BASIC AERODYNAMICS 