跳到主要导航 跳到搜索 跳到主要内容

Shape-preserving mesh deformation method of perforated surfaces and application to double-wall turbine blade leading edge

  • Zhenyuan ZHANG
  • , Honglin LI
  • , Zhonghao TANG
  • , Yajie BAO
  • , Yujie ZHAO
  • , Lei LI
  • Northwestern Polytechnical University Xian

科研成果: 期刊稿件文章同行评审

摘要

A Hybrid Free-Form Deformation (HFFD) method is developed to improve shape preservation in mesh deformation for perforated surfaces, which traditional Free-Form Deformation (FFD) techniques struggle to handle effectively. The proposed method enables high-fidelity parameterized deformation for both flat and curved perforated surfaces while maintaining mesh quality with minimal geometric distortion. To evaluate its effectiveness, comparative studies between HFFD and conventional FFD methods are conducted, demonstrating superior performance in mesh quality and geometric fidelity. The HFFD-based framework is further applied to the Multidisciplinary Design Optimization (MDO) of a double-wall turbine blade leading edge. Results indicate an 11.6 % increase in cooling efficiency and a 16.21 % reduction in maximum stress. Additionally, compared to traditional geometry-based parameterization in MDO, the HFFD approach improves model processing efficiency by 84.15 % and overall optimization efficiency by 20.05 %. These findings demonstrate HFFD's potential to significantly improve complex engineering design optimization by achieving precise shape preservation and improving computational efficiency.

源语言英语
文章编号103728
期刊Chinese Journal of Aeronautics
39
1
DOI
出版状态已出版 - 1月 2026

指纹

探究 'Shape-preserving mesh deformation method of perforated surfaces and application to double-wall turbine blade leading edge' 的科研主题。它们共同构成独一无二的指纹。

引用此