Flowfield visualization of crossing shock-wave/boundary-layer interactions-Reference-Cited by-同舟云学术

Flowfield visualization of crossing shock-wave/boundary-layer interactions

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

GARRISON T.¹,SETTLES G.¹

Affiliation:

1. Pennsylvania State University, University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-750

Reference11 articles.

1. Batcho, P.F., Ketchum, A.C., Bogdonoff, S.M., and Fernando, E.M. "Preliminary Study of the Interactions Caused by Crossing Shock Waves and a Turbulent Boundary Layer," AIAA Paper 89-0359,1989.

2. Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer

3. Hingst,W.R., andWilliams,K.E. "Interaction ofTwo Glancing, Crossing Shock Waves with Turbulent BoundaryLayers at Various Mach Numbers,"NASA TM 103740,1991.

4. Crossing shock wave-turbulent boundary layer interactions

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