nc_derivsΒΆ
Provides non-circulatory aerodynamic lift and moment coefficients derivatives Ref. Palacios and Cesnik, Chap 3.
| param x_ea_perc: | |
|---|---|
| position of axis of rotation in percentage of chord (measured from LE) | |
| param x_fc_perc: | |
| position of flap axis of rotation in percentage of chord (measured from LE) | |