Searched refs:x_probe_wing (Results 1 – 4 of 4) sorted by relevance
93 w_clean_wing = Gamma_clean_wing / (2 * LS_PI * x_probe_wing); in uiuc_betaprobe()94 w_iced_wing = Gamma_iced_wing / (2 * LS_PI * x_probe_wing); in uiuc_betaprobe()
156 x_probe_wing = token_value; in parse_ice()
2264 double x_probe_wing; member2273 #define x_probe_wing aircraft_->x_probe_wing macro
861 ice beta_probe_wing <x_probe_wing> # wing flow angle probe location uiuc_aircraft.h