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Publishing Language: Chinese

Research progress of RBF dynamic mesh technology and its application in aeroelasticity

Chao YANG1,2, Zhicheng ZOU1, Changchuan XIE1,2( ), Chao AN1, Cunyi HU3
School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China
Hangzhou International Innovation Institute, Beihang University, Hangzhou 311115, China
School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China
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Abstract

In multidisciplinary coupled calculations represented by aeroelastic calculations, structural deformation will lead to deformation of the fluid solution domain. It is necessary to develop a dynamic mesh deformation technology with good versatility, high computational efficiency and strong applicability to meet the calculation needs of aerodynamic forces. The dynamic mesh technology based on the Radial Basis Function (RBF) interpolation method has strong deformation ability and is applicable to the deformation calculation of any type of mesh. It is considered to be a dynamic mesh technology with good application prospects. This article introduces the basic theory of dynamic mesh technology based on RBF, and analyzes the selection scheme of basis function and compact radius of RBF. The research progress of acceleration algorithm and accuracy improvement method for mesh deformation technology based on RBF is summarized, and the hybrid dynamic mesh technology based on RBF is introduced. A brief summary of the current research status of RBF-based dynamic mesh technology in aeroelastic calculations is also made.

CLC number: V211.3 Document code: A Article ID: 1000-6893(2025)05-530945-22

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
YANG C, ZOU Z, XIE C, et al. Research progress of RBF dynamic mesh technology and its application in aeroelasticity. Acta Aeronautica et Astronautica Sinica, 2025, 46(5). https://doi.org/10.7527/S1000-6893.2024.30945

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Received: 15 July 2024
Revised: 11 September 2024
Accepted: 18 September 2024
Published: 24 September 2024
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica