Aircraft Aerodynamic Model

Usage Disclaimer

• The effect of the wing's wake on the tail is not modeled. This includes deep stall.
• Tail authority is not modeled past aircraft stall. If the model says the aircraft can pitch up to stall, the aircraft can likely stall itself.
• Static stability is evaluated at 0 AOA.
• The effects of wing sweep become less reliable past 35 degrees, and can be considered inaccurate past 45 degrees.
• Changing the selected input units does not change the value of inputs that have already been typed out.
• High AOA results begin to break down for airfoils of thickness below 9%.
• High AOA wing results break down below roughly AR = 4 and are best used above roughly AR = 5.