Isolator characteristics under steady and oscillatory back pressures-Reference-Cited by-同舟云学术

Isolator characteristics under steady and oscillatory back pressures

Published:2020-09-01 Issue:9 Volume:32 Page:096104
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

R. Saravanan¹,Desikan S. L. N.¹^ORCID,T. M. Muruganandam²

Affiliation:

1. Wind Tunnel Data Division, Aeronautics Entity, Vikram Sarabhai Space Centre, Thiruvananthapuram 695022, India

2. Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0016360

Reference21 articles.

1. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview

2. Shock train and pseudo-shock phenomena in internal gas flows

3. J. Dutton and B. Carroll, “Numerical and experimental investigation of multiple shock wave/turbulent boundary layer interactions in a rectangular isolator,” Technical Report No. AD-A190-772, U.S. Air Force Office of Scientific Research, University of Illinois, Urbana, IL, 1988.

4. Turbulence phenomena in a multiple normal shock wave/turbulent boundary-layer interaction

5. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

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