Experimental Investigation of 3D Shock / Boundary Layer Interaction Control in Transonic Flows-Reference-Cited by-同舟云学术

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Experimental Investigation of 3D Shock / Boundary Layer Interaction Control in Transonic Flows

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

Ogawa Hideaki¹,Babinsky Holger¹

Affiliation:

1. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-879

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental FSI study of adaptive shock control bumps;Journal of Fluids and Structures;2018-08

2. Review of research into shock control bumps;Shock Waves;2014-10-28

3. Three-dimensional shock control bumps: effects of geometry;52nd Aerospace Sciences Meeting;2014-01-10

4. Numerical and Experimental Examination of Shock Control Bump Flow Physics;High Performance Computing in Science and Engineering ‘12;2012-10-22

5. Experimental Study on Pressure Fluctuations in the Shock/boundary Layer Interaction of an Axisymmetric Body;Applied Mechanics and Materials;2011-07

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