Parametric modeling of turbine cooling blades
It is now possible to automatically optimize the cooling structure and cooling performance in conjunction with changes to the blade shape!
The blades used in aircraft engines and gas turbines become very hot, so cooling air is supplied to the countless holes on the blade surface through cooling passages provided inside the blades. In conventional design methods, automatic optimization was considered difficult due to the complexity of shapes, robustness of mesh generation, and computation time. However, this case presents an example of fully automated optimization using CAESES. *For more detailed information, please refer to the related links. For further details, you can download the PDF or feel free to contact us.*
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*You can view the detailed content of the article through the related link. For more information, please download the PDF or feel free to contact us.*
