This package allows efficient computation of nonlinear aerodynamic properties of a wing. It employs 2D section data to build a 3D potential vortex model of the flow. It uses a robust Euler-Newton method to track the change of flow vorticity quantities as the angle of attack progresses.
released on 2 March 2009
- Octave-data smoothing
|License||Verified by||Verified on||Notes|
|GPLv3orlater||Kelly Hopkins||28 July 2009|
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This entry (in part or in whole) was last reviewed on 17 January 2017.
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