Panel method for the simulation of the performance of a biplane

Version 1.0.0.0 (5,39 KB) von Alexander Giles
Doublet and source formulation (Dirichlet boundary condition)
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Aktualisiert 31. Aug 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.

Zitieren als

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. Abgerufen .

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Erstellt mit R2014b
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Version Veröffentlicht Versionshinweise
1.0.0.0