A Simulation Scheme of the Grid Strategy Parameters Based on the NACA0012 Airfoil at the Hypersonic Speed

Ke Deng, Jinping Li, Gang Wang, Guangming Zhang, Zhiqing Bai, Lu Yang

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

At present, the simulation scheme of grid strategy parameters at hypersonic speed is a hot topic and can be applied to the NACA0012 airfoil, but the selection criteria for Reynolds number and aspect ratio near impact are relatively few, and further research is needed. In this paper, using the NACA4 digital generator airfoil modeling method, a two-dimensional outflow field based on the sharp trailing edge NACA0012 is established. Simulation calculations obtain the numerical results. Through comparison with the reference data, a grid strategy parameters simulation scheme is presented. Unlike blunt bodies, the longitudinal and transverse ratios between cell Reynolds number and cells near impact should be no greater than 16 and 240, respectively.

源语言英语
主期刊名International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023
编辑Xin Feng, Aniruddha Bhattacharjya
出版商SPIE
ISBN(电子版)9781510665040
DOI
出版状态已出版 - 2023
活动2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023 - Guangzhou, 中国
期限: 17 2月 202319 2月 2023

出版系列

姓名Proceedings of SPIE - The International Society for Optical Engineering
12645
ISSN(印刷版)0277-786X
ISSN(电子版)1996-756X

会议

会议2023 International Conference on Computer, Artificial Intelligence, and Control Engineering, CAICE 2023
国家/地区中国
Guangzhou
时期17/02/2319/02/23

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