Fluctuating wall pressures near separation in highly swept turbulent interactions-Reference-Cited by-同舟云学术

Fluctuating wall pressures near separation in highly swept turbulent interactions

Published:1994-06 Issue:6 Volume:32 Page:1151-1157
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Schmisseur J. D.¹,Dolling D. S.²

Affiliation:

1. Wright-Patterson Air Force Base, Dayton, Ohio 45433

2. University of Texas at Austin, Austin, Texas 78712

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.12114

Reference19 articles.

1. Swept shock/boundary-layer interactions - Tutorial and update

2. Structure of swept shock wave/boundary-layer interactions using conical shadowgraphy

3. Physical model of the swept shock wave/boundary-layer interaction flowfield

4. On the quasi-conical flowfield structure of the swept shock wave-turbulent boundary layer interaction

5. 5Tran, T. T. "An Experimental Investigation of Unsteadiness in Swept Shock Wave/Turbulent Boundary Layer Interactions," Ph.D. Dissertation, Mechanical and Aerospace Engineering Dept.Princeton Univ., Princeton, NJ,March 1987.

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