Relationship Between Intermittent Separation and Vortex Structure in a Three-Dimensional Shock/Boundary-Layer Interaction-Reference-Cited by-同舟云学术

Relationship Between Intermittent Separation and Vortex Structure in a Three-Dimensional Shock/Boundary-Layer Interaction

Published:2016-06 Issue:6 Volume:54 Page:1862-1880
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Morajkar Rohan R.¹,Klomparens Robin L.¹,Eagle W. Ethan¹,Driscoll James F.¹,Gamba Mirko¹,Benek John A.²

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109

2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053905

Reference64 articles.

1. A simple model for low-frequency unsteadiness in shock-induced separation

2. Effect of Interaction Strength on Unsteadiness in Shock-Wave-Induced Separations

3. Vortex identification: New requirements and limitations

4. Shock wave–boundary layer interactions in rectangular inlets: three-dimensional separation topology and critical points

5. EagleW. E. “An Experimental Study of Three-Dimensional Inlet Shock-Boundary Layer Interactions,” Ph.D. Thesis, Univ. of Michigan, Ann Arbor, MI, 2012.

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