Panel method for NACA XXXX aerofoils

版本 1.0.0.0 (5.2 KB) 作者: Alexander Giles
Panel method using doublets and sources with the Dirichlet boundary condition
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更新时间 2015/8/31

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Following the implementation of Katz and Plotkin, this code simulates the performance of an aerofoil in steady flow assuming that the flow remains attached and viscous effects can be ignored.

引用格式

Alexander Giles (2024). Panel method for NACA XXXX aerofoils (https://www.mathworks.com/matlabcentral/fileexchange/52771-panel-method-for-naca-xxxx-aerofoils), MATLAB Central File Exchange. 检索来源 .

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版本 已发布 发行说明
1.0.0.0