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Airfoil Aerodynamics Using Panel Methods

2008
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The Mathematica Journal
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Potential flow over an airfoil plays an important historical role in the theory of flight. The governing equation for potential flow is Laplace's equation, a widely studied linear partial differential equation. One of Green's identities can be used to write a solution to Laplace's equation as a boundary integral. Numerical models based on this approach are known as panel methods in the aerodynamics community. This article introduces the availability of a collection of computational tools for

doi:10.3888/tmj.10.4-6
fatcat:6qrc7rd2rbdvva4wip5vdp7g7y