AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
PDF (6.1 MB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Research Article | Publishing Language: Chinese | Open Access

Initial discontinuity induced non-physical fluctuation and its elimination algorithm

Jun LIU1( )Fang HAN1Yixuan SUN2Yu LIU3
School of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024, China
Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China
Faculty of Mechanical Engineering & Mechanics, Ningbo University, Ningbo 315211, China
Show Author Information

Abstract

When the shock capturing method is used to solve inviscid compressible flow with a mathematical discontinuity as the initial condition, the discontinuity will gradually evolve into a numerical transition region across several grid points, and non-physical fluctuations in two directions parallel to the discontinuity can be induced in this process. The initial shock, which is calculated as the initial condition, satisfies the Euler equation, while the flow field parameters should satisfy the modified equations, such conflict might be the reason for the initial shock-induced non-physical fluctuations. As the discontinuities such as shock waves are defined by the characteristic lines of the Euler equation, an upwind flux scheme based on characteristics (UFSC) is proposed in the present study. Using several conventional conservation flux schemes as a reference, the UFSC can eliminate the non-physical fluctuations induced by the Steger-Warming and Van Leer schemes at the initial contact discontinuities, and can reduce the amplitude of the initial shock-induced disturbances. For the flow field in smooth regions, the computational results from the UFSC and conserved flux scheme are similar, but larger pressure peaks appear near the strong shock. To overcome this defect, a hybrid scheme UFSC+S is constructed, which uses the Steger-Warming for calculation in the shock region and the UFSC in other regions.

CLC number: V211.3; O354.5 Document code: A

References

【1】
【1】
 
 
Acta Aerodynamica Sinica
Pages 18-32

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
LIU J, HAN F, SUN Y, et al. Initial discontinuity induced non-physical fluctuation and its elimination algorithm. Acta Aerodynamica Sinica, 2024, 42(11): 18-32. https://doi.org/10.7638/kqdlxxb-2023.0203

430

Views

4

Downloads

0

Crossref

2

Scopus

0

CSCD

Received: 26 October 2023
Revised: 25 February 2024
Published: 05 August 2024
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).