Panel method for the simulation of the performance of a biplane
Version 1.0.0.0 (5.39 KB) by
Alexander Giles
Doublet and source formulation (Dirichlet boundary condition)
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
Platform Compatibility
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Version | Published | Release Notes | |
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1.0.0.0 |