TSFOIL Analysis Interface Module (AIM)
TSFOIL Analysis Interface Module (AIM)
AIM Outputs
The following list outlines the TSFOIL outputs available through the AIM interface.
CL =
Coefficient of lift value.
CD =
Coefficient of drag value. (Calculated from momentum integral)
CD_Wave =
Wave drag coefficient value.
CM =
Moment coefficient value.
Cp_Critical =
Critical pressure coefficient (M = 1).
Generated on Fri Feb 28 2025 09:07:03 for TSFOIL Analysis Interface Module (AIM) by
1.9.1
1.9.1