Experiments in Unsteady Forcing of Mach 2 Shock Wave/Boundary Layer Interactions-Reference-Cited by-同舟云学术

Experiments in Unsteady Forcing of Mach 2 Shock Wave/Boundary Layer Interactions

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Bueno Pablo¹,Wagner Justin¹,Searcy J.¹,Ganapathisubramani B.¹,Clemens Noel¹,Dolling David¹

Affiliation:

1. University of Texas

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-878

Reference15 articles.

1. Relationship Between Upstream Turbulent Boundary-Layer Velocity Fluctuations and Separation Shock Unsteadiness

2. Effects of Boundary-Layer Velocity Fluctuations on Unsteadiness of Blunt-Fin Interactions

3. 3Hou, Y. X. "Particle Image Velocimetry Study of Shock Induced Turbulent Boundary Layer Separation", Ph.D. Dissertation, Dept.ofAerospace EngineeringandEngineeringMechanics,TheUniversityofTexasat Austin, Austin, TX,2003.

4. Large-scale motions in a supersonic turbulent boundary layer

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