nc_derivsΒΆ
Provides non-circulatory aerodynamic lift and moment coefficients derivatives Ref. Palacios and Cesnik, Chap 3.
param x_ea_perc: | |
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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) |