Here, NEWPAN is compared against experimental data from NASA.
William P. Henderson, "Effects of wing leading-edge radius and
Reynolds number on longitudinal aerodynamic characteristics of highly
swept wing-body configurations at subsonic speeds" - NASA TN D-8361, 1976
The basic geometry is illustrated here via the surface panelling.
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Results for Cl, Cd, Cm are shown for an incidence sweep.
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