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Journal of System Simulation

Abstract

Abstract: The solution of the coupling characteristics of fluid-thermo-solid physics in the modeling of hypersonic vehicle is an unavoidable difficulty, and the real-time simulation of fluid-thermo-solid coupling is particularly challenging. Aiming at the conflicting problem of solution accuracy and solution efficiency in fluid-thermo-solid coupling real-time simulation, a CFD (Computational Fluid Dynamics)/ CSD (Computational Structural Dynamics)-based fluid-thermo-solid coupling characteristic solution method is established, which realizes the high-precision solution of the fluid, temperature, and structural deformation field coupling. According to the multi-condition offline solution set modeling method, by accumulating a large number of offline solutions as effective support for online calculation, the contradiction between solution accuracy and solution efficiency is balanced. A virtual flight test is carried out to analyze the influence of the coupling effect on the angle of attack and net thrust of the aircraft, and compared with NASA experimental data to verify the correctness of the model.

First Page

2820

Revised Date

2021-08-18

Last Page

2827

CLC

TP391.9

Recommended Citation

Liu Yunqin, Li Ni, Zhao Luming, Bai Jinpeng, Li Tingjun, Wang Chenguang. Real-time Simulation Technology of Fluid-thermo-solid Coupling of Hypersonic Vehicle[J]. Journal of System Simulation, 2021, 33(12): 2820-2827.

DOI

10.16182/j.issn1004731x.joss.21-FZ0838

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