Linear analysis on pressure-dilatation behind shock waves
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Connecticut 1 , Storrs, Connecticut 06269, USA
2. Department of Aerospace Engineering, Texas A&M University 2 , College Station, Texas 77843, USA
Abstract
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://pubs.aip.org/aip/pof/article-pdf/doi/10.1063/5.0138476/16661282/021701_1_online.pdf
Reference32 articles.
1. H. S. Ribner, “Convection of a pattern of vorticity through a shock wave,” Report No. NACA TR-1164 (NACA, 1954).
2. H. S. Ribner, “Shock-turbulence interaction and the generation of noise,” Report No. NACA TR-1233 (NACA, 1954).
3. F. K. Moore, “Unsteady oblique interaction of a shock wave with a plane disturbance,” Report No. NACA 1165 (NACA, 1954).
4. Turbulence amplification in shock-wave boundary-layer interaction;AIAA J.,1982
5. Interaction of an isotropic field of acoustic waves with a shock wave;J. Fluid Mech.,1995
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