Parametric uncertainty quantification of SST turbulence model for a shock train and pseudo-shock phenomenon-Reference-Cited by-同舟云学术

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Parametric uncertainty quantification of SST turbulence model for a shock train and pseudo-shock phenomenon

Published:2022-07 Issue: Volume:196 Page:290-302
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Zeng Fan-zhi^ORCID,Li Jin-ping^ORCID,Wang Yu^ORCID,Sun Mao,Yan Chao^ORCID

Funder

National Natural Science Foundation of China

National Numerical Wind Tunnel Project of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. Numerical and Experimental Investigation of Multiple Shock Wave/turbulent Boundary Layer Interactions in a Rectangular Duct;Carroll,1988

2. Shock train and pseudo-shock phenomena in internal gas flows;Matsuo;Prog. Aero. Sci.,1999

3. Pseudo-shock waves and their interactions in high-speed intakes;Gnani;Prog. Aero. Sci.,2016

4. Supersonic diffusers for wind tunnels;Neumann;J. Appl. Mech.,1949

5. Turbulence phenomena in a multiple normal shock wave/turbulent boundary-layer interaction;Carroll;AIAA J.,1992

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