Searched refs:CL_right (Results 1 – 3 of 3) sorted by relevance
146 SCALAR CL_left, CL_cent, CL_right; // CL values across the span in basic_aero() local338 CL_right = CL_0 + CL_a*(Std_Alpha - Alpha_0 + Phat*eta_loc); in basic_aero()360 if (CL_right > CL_max) in basic_aero()362 dCL_right = CL_max-CL_right -CL_drop; in basic_aero()378 if (CL_right < CL_min) in basic_aero()380 dCL_right = CL_min-CL_right -CL_drop; in basic_aero()
444 SCALAR CL_left, CL_cent, CL_right; // CL values across the span in aero() local515 CL_right = CL_0 + CL_a*(Alpha - Alpha_0 + Phat*eta_loc) + CL_offset; in aero()544 if (CL_right > CL_max_flap) in aero()546 dCL_right = CL_max_flap - CL_right - CL_drop; in aero()559 if (CL_right < CL_min_flap) in aero()561 dCL_right = CL_min_flap - CL_right - CL_drop*CL_min/CL_max; in aero()568 + 0.25*(CL_left + dCL_left) + 0.25*(CL_right + dCL_right); in aero()
658 SCALAR CL_left, CL_cent, CL_right; // CL values across the span in aero() local744 CL_right = CL_0 + CL_a*(Alpha - Alpha_0 + Phat*eta_loc); in aero()764 if (CL_right > CL_max) in aero()766 dCL_right = CL_max-CL_right -CL_drop; in aero()782 if (CL_right < CL_min) in aero()784 dCL_right = CL_min-CL_right -CL_drop; in aero()