Panel method for the simulation of the performance of a biplane

Doublet and source formulation (Dirichlet boundary condition)
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Updated Mon, 31 Aug 2015 14:43:37 +0000

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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.

Cite As

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. Retrieved .

MATLAB Release Compatibility
Created with R2014b
Compatible with any release
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Version Published Release Notes
1.0.0.0