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Open Access

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

Zhenyuan ZHANGa, Honglin LIa, Zhonghao TANGb, Yajie BAOa, Yujie ZHAOa, Lei LIa( )
Department of Engineering Mechanics, Northwestern Polytechnical University, Xi’an 710072,China
School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710129,China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

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.

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Chinese Journal of Aeronautics

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Cite this article:
ZHANG Z, LI H, TANG Z, et al. Shape-preserving mesh deformation method of perforated surfaces and application to double-wall turbine blade leading edge. Chinese Journal of Aeronautics, 2026, 39(1). https://doi.org/10.1016/j.cja.2025.103728

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Received: 12 November 2024
Revised: 28 November 2024
Accepted: 20 March 2025
Published: 28 July 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).