A question about airfoil optimization using Genetic Algorithm
显示 更早的评论
For Airfoil optimization using genetic algorithm .. How can I obtain a equation that Links my control points of the airfoil to the objectives like cl and cd .. I really don't know how to link them together through equation or implement Control points in the objective function
回答（3 个）
Alan Weiss
2016-9-19
编辑：Alan Weiss
2016-9-19
0 个投票
I really don't know anything about Simulink though, so will not be able to provide any further help.
Alan Weiss
MATLAB mathematical toolbox documentation
Fernando Echeverria
2016-11-11
0 个投票
Hello,
I think you should go outside Matlab in the middle. You need to link your Matlab code to a panel method code or CFD: Change the geometry in Matlab, feed the aerodynamic code, launch it and read the solution in Matlab.
Best regards
yassine khalil
2017-1-26
0 个投票
You can use XFOIL as script in Matlab. XFOIL is able to generate the Cl and Cd and then the objective function
1 个评论
Hesham Shaarawy
2021-1-30
Can you please elaborate on how XFOIL can provide the objective function, once the Cl and Cd have been obtained ?
类别
在 帮助中心 和 File Exchange 中查找有关 Airfoil tools 的更多信息
2016-9-19
2021-1-30
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!
Translated by 
