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Open Access

A new accelerating technique for low speed flow: Pseudo high speed method

Haitao DONGaFujun LIUb( )
NLCFD, School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China
China Aerodynamic Research and Development Center, Mianyang 621000, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

This paper proposes a new accelerating technique for simulating low speed flows, termed as pSeudo High Speed method (SHS), which uses governing equations and numerical methods of compressible flows. SHS method has advantages of simple formula, easy manipulation, and only need to modify flux of Euler equations. It can directly employ the existing well-developed schemes of hyperbolic conservation laws. To verify the technique, several numerical experiments are performed, such as: flow past airfoils and flow past a cylinder. Analysis of SHS method and comparisons with some precondition methods are made numerically. All tests show that SHS method can greatly improve the efficiency of compressible method simulating low speed flow fields, which exhibits in accelerating the convergence rate and increasing the accuracy of the numerical results.

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Chinese Journal of Aeronautics
Pages 45-64

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Cite this article:
DONG H, LIU F. A new accelerating technique for low speed flow: Pseudo high speed method. Chinese Journal of Aeronautics, 2022, 35(8): 45-64. https://doi.org/10.1016/j.cja.2021.10.018

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Received: 09 March 2020
Revised: 29 June 2021
Accepted: 03 August 2021
Published: 01 December 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/).