Paper
23 May 2023 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
Author Affiliations +
Proceedings Volume 12645, International Conference on Computer, Artificial Intelligence, and Control Engineering (CAICE 2023); 126454N (2023) https://doi.org/10.1117/12.2681299
Event: International Conference on Computer, Artificial Intelligence, and Control Engineering (CAICE 2023), 2023, Hangzhou, China
Abstract
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.
© (2023) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Ke Deng, Jinping Li, Gang Wang, Guangming Zhang, Zhiqing Bai, and Lu Yang "A simulation scheme of the grid strategy parameters based on the NACA0012 airfoil at the hypersonic speed", Proc. SPIE 12645, International Conference on Computer, Artificial Intelligence, and Control Engineering (CAICE 2023), 126454N (23 May 2023); https://doi.org/10.1117/12.2681299
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KEYWORDS
Computer simulations

Turbulence

Viscosity

Numerical simulations

Design and modelling

Modeling

Numerical analysis

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