NAVWEPS 00-BOT-80 
HIGH SPEED AERODYNAMICS 
CONE IN SUPERSONIC FLOW 
CONICAL WAVE 
REF:LECTED OBLIOUE WAVES 
MODEL IN WIND 
TUNNEL WITH wows 
REFL\Cmg FROM 
Figure 3.5. Three Dimensional and Reflected Shock Waves 
209 Revised Januaty I%5