The following list outlines the FlightStream outputs available through the AIM interface. All variables currently correspond to values found in the *.plt file

Aerodynamic coefficients:

• Cx = X-force coefficient
• Cx = X-force coefficient
• Cx = X-force coefficient
• CL = Lift coefficient
• CD = drag coefficient
• CMx = X-moment coefficient
• CMy = Y-moment coefficient
• CMz = Z-moment coefficient