Aerodynamic and topology optimizaiton

Version 1.0.0 (7.89 KB) by volkan P
This code optimizes RAE 2822 airfoil under aerodynamic and structural concrens.
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Updated 9 Mar 2023

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The presented code is composed of aerodynamic and structural parts. The aerodynamic part is based on shape optimizaiton under drag to lift ratio concern. The structural part is governed by von Mises stress and weight. Both objectives are minimized by using genetic algorithm. An additional code, finvol.exe, required for flow simulation is available if requested.

Cite As

volkan P (2025). Aerodynamic and topology optimizaiton (https://ch.mathworks.com/matlabcentral/fileexchange/125940-aerodynamic-and-topology-optimizaiton), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2022b
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.0.0