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