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  Revised Januaty I%5  209 