Searched refs:beta_flow_iced_tail (Results 1 – 4 of 4) sorted by relevance
121 beta_flow_iced_tail = asin((w_iced_tail / V_total_iced_tail) * in uiuc_betaprobe()125 Dbeta_flow_tail = fabs(beta_flow_clean_tail - beta_flow_iced_tail); in uiuc_betaprobe()128 pct_beta_flow_tail = beta_flow_iced_tail / beta_flow_clean_tail; in uiuc_betaprobe()
1813 fout << beta_flow_iced_tail << " "; in uiuc_recorder()1818 fout << beta_flow_iced_tail * RAD_TO_DEG << " "; in uiuc_recorder()
2874 double beta_flow_iced_tail, beta_flow_iced_tail_deg; member2881 #define beta_flow_iced_tail aircraft_->beta_flow_iced_tail macro
1050 record beta_flow_iced_tail # [rad] tail iced flow angle uiuc_aircraft.h