Wall pressure fluctuations beneath swept shock wave/boundary layer interactions-Reference-Cited by-同舟云学术

Wall pressure fluctuations beneath swept shock wave/boundary layer interactions

Published:1993-01-11 Issue: Volume: Page:
ISSN:
Container-title:31st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

GARG S.¹,SETTLES G.¹

Affiliation:

1. Pennsylvania State Univ., University Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-384

Reference20 articles.

1. Lu, F. K. "Fin Generated Shock-Wave Boundary-LayerInteractions," Ph.D. Dissertation,Mechanical Engineering Dept.The Pennsylvania State University, Feb. 1988.

2. Kim, K. S. "Skin FrictionMeasurements by Laser Interferometry in Supersonic Flows," Ph.D. Dissertation, Mechanical Engineering Dept.The Pennsylvania StateUniversity, Dec. 1988.

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

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