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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 NASA experimental data.
John W. Boyd, "Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds" - NASA RM A52D01c, 1952

Results for Cl, Cd, Cm are shown for an incidence sweep, for different flap angle deflections

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