Panel method for the simulation of the performance of a biplane

Versione 1.0.0.0 (5,39 KB) da Alexander Giles
Doublet and source formulation (Dirichlet boundary condition)
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Aggiornato 31 ago 2015

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Illustrates the effect of having multiple lifting elements in the flow. Kutta condition is applied separately to each element's trailing edge.

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Alexander Giles (2024). Panel method for the simulation of the performance of a biplane (https://www.mathworks.com/matlabcentral/fileexchange/52772-panel-method-for-the-simulation-of-the-performance-of-a-biplane), MATLAB Central File Exchange. Recuperato .

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Versione Pubblicato Note della release
1.0.0.0