Searched refs:KCm_de (Results 1 – 1 of 1) sorted by relevance
29 double KCm_de; in Calc_Iced_Forces() local77 KCm_de = delta_Cm_de/eta_ref_tail; in Calc_Iced_Forces()78 delta_Cm = (0.75*eta_wing + 0.25*eta_tail)*KCm_alpha + (eta_tail)*KCm_de; in Calc_Iced_Forces()