NAVWEPS 00-801-80  HIGH SPEED AERODYNAMICS  APPROXIMATE VARIATION OF CRITICAL  i.oo-  MACH NUMBER WITH ASPECT RATIO FOR  A 9% THICK AIRFOIL  SECTION  .95-  CRITICAL  .90-  MACH  .85-  NUMBER  MCR  .80-  .75 -  .7od  I  1  1  I  1  9  I  01  2  3  4  5  6  7  8  IO  II  I2  ASPECT RATIO, AR  MACH CONES FORMED AT  TIPS OF RECTANGULAR  \-  WING IN SUPERSONIC FLOW  PRESSURE DISTRIBUTION  AT THE TIP OF THE  RECTANGULAR WING  Y-  MACH CONE  VORTEX CREATED WITHIN  THE MACH CONE AT THE TIP  OF THE RECTANGULAR WING  WING WITH TIPS  “RAKED” OUTSIDE  THE TIP CONES  Figure 3.18. Generd Pknform Effects  235 