TSFOIL Analysis Interface Module (AIM)
TSFOIL Analysis Interface Module (AIM)
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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 Wed Sep 17 2025 23:46:24 for TSFOIL Analysis Interface Module (AIM) by
1.9.8
1.9.8