Multidisciplinary Design Optimization of Cooling Turbine Blade: An Integrated Approach with R/ICSM
Wenjun Wang,
Lan Xiang,
Enzi Kang
et al.
Abstract:This paper presents an efficient integrated multidisciplinary design optimization method for shaping a high-pressure cooling turbine blade in aero engines. This approach utilizes a novel regression/interpolation combination surrogate model (R/ICSM), facilitating comprehensive design optimization through collaborative coupling feature parameterization modeling and numerical simulation analysis across various disciplines. The optimized blade adjusts the load distribution on its surface, effectively eliminating f… Show more
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