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| Overview | | High Lift Validation | | Compressibility Validation | | Unsteady Validation(1) | | Unsteady Validation(2) | | Low AR Validation | | Low AR Validation(2) |
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.

Results for Cl, Cd, Cm are shown for an incidence sweep.

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