Searched refs:w_iced_tail (Results 1 – 4 of 4) sorted by relevance
96 w_iced_tail = Gamma_iced_tail / (2 * LS_PI * x_probe_tail); in uiuc_betaprobe()110 V_total_iced_tail = sqrt(w_iced_tail*w_iced_tail + in uiuc_betaprobe()112 2*w_iced_tail*V_rel_wind * in uiuc_betaprobe()121 beta_flow_iced_tail = asin((w_iced_tail / V_total_iced_tail) * in uiuc_betaprobe()
1758 fout << w_iced_tail << " "; in uiuc_recorder()
2860 double w_clean_tail, w_iced_tail; member2864 #define w_iced_tail aircraft_->w_iced_tail macro
1039 record w_iced_tail # [ft/s] tail iced downwash uiuc_aircraft.h