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Open Access

A learning-based approach for solving shear stress vector distribution from shear-sensitive liquid crystal coating images

Jisong ZHAOa( )Jinming ZHANGa,bBoqiao WANGa,b
College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Faculty of Rocket and Space Technology, Kharkiv Aviation Institute, National Aerospace University, Kharkiv 61070, Ukraine

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

A learning-based approach for solving wall shear stresses from Shear-Sensitive Liquid Crystal Coating (SSLCC) color images is presented in this paper. The approach is able to learn and establish the mapping relationship between the SSLCC color-change responses in different observation directions and the shear stress vectors, and then uses the mapping relationship to solve wall shear stress vectors from SSLCC color images. Experimental results show that the proposed approach can solve wall shear stress vectors using two or more SSLCC images, and even using only one image for symmetrical flow field. The accuracy of the approach using four or more observations is found to be comparable to that of the traditional multi-view Gauss curve fitting approach; the accuracy is slightly reduced when using two or fewer observations. The computational efficiency is significantly improved when compared with the traditional Gauss curve fitting approach, and the wall shear stress vectors can be solved in nearly real time. The learning-based approach has no strict requirements on illumination direction and observation directions and is therefore more flexible to use in practical wind tunnel measurement when compared with traditional liquid crystal-based methods.

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Chinese Journal of Aeronautics
Pages 55-65

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Cite this article:
ZHAO J, ZHANG J, WANG B. A learning-based approach for solving shear stress vector distribution from shear-sensitive liquid crystal coating images. Chinese Journal of Aeronautics, 2022, 35(4): 55-65. https://doi.org/10.1016/j.cja.2021.04.019

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Received: 26 November 2020
Revised: 25 December 2020
Accepted: 13 January 2021
Published: 26 May 2021
© 2021 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/).