- Low-order model of an unsteady streamwise gust interaction with a flat plate
- Based on classical aerodynamic results
- Circulatory force history from Wagner (see Principles of Helicopter Aerodynamics - G. Leishman)
- Non-circulatory forces from analytic treatment of added-mass
- An iterative solver is used to mitigate the effect of streamwise gusts (i.e. solving for the angle of attack that produces a given lift)
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Low-order model of an unsteady streamwise gust based on classical aerodynamic results.
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