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

Reiterate inputs (based on cases):

• Beta = Sideslip [degree].
• Alpha = Angle of attack [degree].
• Dynamic_Pressure = Dynamic pressure [bar].
• Mach = Mach number.

Per-Trb:

• PerTrb = PerTrb.

Net Forces - Pressure + Viscous:

• CLtot = The lift coefficient.
• CDtot = The drag coefficient.
• CMYtot = The moment coefficient about the y-axis.
• LoDtot = Lift to drag ratio.

Pressure Forces:

• CL_p = The lift coefficient - pressure contribution only.
• CD_p = The drag coefficient - pressure contribution only.

Viscous Forces:

• CL_v = The lift coefficient - viscous contribution only.
• CD_v = The drag coefficient - viscous contribution only.

Aero-thermal:

• Stagnation_Temperature = Stagnation temperature [K].
• Stagnation_Radius = = Stagnation radius [m].
• Convective_Flux = Convective heat flux [W/cm²].
• Radiative_Flux = Radiation heat flux [W/cm²].

Trefftz:

• CL_Trefftz = Trefftz lift coefficient.
• CD_Trefftz = Trefftz drag coefficient.