NAVWEPS 00-8OY-60  HIGH SPEED AERODYNAMICS  MAXIMUM LOCALVELOCITY  M=.50  IS LESS THAN SONIC  MAXIMUM LOCAL VELOCITY  EOUALTO SONIC  M =.72  (CRITICAL MACH NUMB  NORMAL SHOCK WAVE  POSSIBLE SEPARATION  su  NORMAL SHOCK  \\I  NORMAL SHOCK  NORMAL SHOCK  Figure 3.9. Transonic Flow Patterns (sheet 1 of 2)  216 