项目描述 ：
MATLAB/Python based solver to optimize 2D airfoil shape with realistic thickness for structural objective functions (polar moment, max. von-Mises stress, volume) and given aerodynamic constraints.

高级语言： MATLAB

项目主页：

项目地址: git://github.com/yajatvp/shape_optmization.git

创建时间： 2020-11-15T17:51:30Z
项目社区：https://github.com/yajatvp/shape_optmization
开源协议：GNU General Public License v3.0
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