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Full Length Article | Open Access

A novel subset assignment and matching method for DIC measurement of complex deformation in aircraft braking process

Xin SHIa,bXiang GUOa,b,( )Tao SUOa,b,cYingtao YUANa,bHongli HEdZhiyong RENd
School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China
International Research Laboratory of Impact Dynamics and its Engineering Application, Xi’an 710072, China
Institute of Extreme Mechanics, Northwestern Polytechnical University, Xi’an 710072, China
Chinese Flight Test Establishment, Xi’an 710089, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

This paper proposes a measurement method related to the braking deformation of a complex motion. During the braking process, the deformation of the wheel includes large amounts of movement, vibration, warping, and distortion. A novel subset assignment and correlation method is proposed to measure the complex deformation. The proposed method can greatly improve the accuracy and stability of the calculation of complex deformations by simplifying the complex deformation into translational deformations in logarithmic coordinate system. According to the simulation and actual experiments, the proposed method can be utilized to measure the deformations of up to 100% tensile strain under complex deformation. According to the accuracy verification experiment, the error of the proposed method is less than 50 με. The results show that the proposed method can effectively carry out structural deformation measurement in the complex motion and deformation process. The proposed method has great significance for structural performance analysis and optimization design considering complex motion and deformation.

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Chinese Journal of Aeronautics
Pages 373-387
Cite this article:
SHI X, GUO X, SUO T, et al. A novel subset assignment and matching method for DIC measurement of complex deformation in aircraft braking process. Chinese Journal of Aeronautics, 2024, 37(8): 373-387. https://doi.org/10.1016/j.cja.2024.02.003

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Received: 10 September 2023
Revised: 06 November 2023
Accepted: 05 February 2024
Published: 07 March 2024
© 2024 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/).

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