The aerodynamic forces are calculated with the prescribed apparent speed but it should be with a relative apparent speed corrected for the sweep, as implemented in the thesis.
No need to output alpha_corrected or uncorrected, only gamma_dist. Everything else can be calculated in wing aero
The aerodynamic forces are calculated with the prescribed apparent speed but it should be with a relative apparent speed corrected for the sweep, as implemented in the thesis.
No need to output alpha_corrected or uncorrected, only gamma_dist. Everything else can be calculated in wing aero