The following list outlines the FlightStream outputs available through the AIM interface.

Analysis settings:

• Alpha = Angle of attack
• Beta = Sideslip angle
• Mach = Fresstream mach
• Velocity = Fresstream velocity
• Density = Fresstream density
• Pressure = Fresstream pressure
• SonicSpeed = Fresstream speed of sound
• Temperature = Fresstream temperature
• Viscosity = Fresstream viscosity

Aerodynamic coefficients:

• Cx = X-force coefficient
• Cx = X-force coefficient
• Cx = X-force coefficient
• CL = Lift coefficient
• CDi = Induced drag coefficient
• CDo = Skin friction drag coefficient
• CMx = X-moment coefficient
• CMy = Y-moment coefficient
• CMz = Z-moment coefficient

NOTE: Coefficients are normalized by the input reference velocity, not the freestream velocity.

Component aerodynamic coefficients are also available as dynamic outputs for a single point analysis.