NAVWEPS 00-801-60 
HIGH SPEED AERODYNAMICS 
DELTA WING PLANFORM 
-PRESSURE 
DISTRIBUTION 
MACH CONE MACH CONE 
AHEAD OF LEADING 
EDGE 
CONTFOL SURFACE 
FLOW PATTERNS 
SONIC FLOW ON 
G EDGE CONTROLS 
M=.85 
SUPERSONIC FLOW CONDITIONS 
TRAILING ED 
CONTROLSURFACE 
Figure 3.19. Planform Effects and Control Surfaces