Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions-Reference-Cited by-同舟云学术

Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions

Published:2018-04 Issue:4 Volume:56 Page:1588-1599
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Combs Christopher S.¹,Lash E. Lara¹,Kreth Phillip A.¹,Schmisseur John D.¹

Affiliation:

1. University of Tennessee Space Institute, Tullahoma, Tennessee 37388

Funder

Office of Naval Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056553

Reference33 articles.

1. KnightD. D.DegrezG. “Shock Wave Boundary Layer Interactions in High Mach Number Flows: A Critical Survey of Current Numerical Prediction Capabilities,” AGARD, Advisory Rept. 319, Vol. 2, 1998, pp. 1.1–1.35.

2. A review of aerothermal problems associated with hypersonic flight

3. Progress in shock wave/boundary layer interactions

4. Shock wave boundary layer interaction

5. Interactions between shock waves and turbulent boundary layers

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