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RESULTS AND DISCUSSION
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A R P Aerodynamic Analysis Mach pressure angle of attack Angle of Normal bal integ press body Chordwise Pressure Distributions coefficient comparisons Concluded configuration correction deg bal integ Dynamic Angle edge effects Figure Flat wing FLEXSTAB flow Fu Lu full span isobars l l º leading leading-edge lift load Loc A L lºquunu Mach numbers methods Normal force Pitching O I O ºssaud Panels Pitching moment Analysis points predict RAct Round L.E. round L.E. L.E. deflection separation span T.E. deflection sw ARP T.E. Deflection Table theoretical theory Twisted wing vortex w f l