Vortical structures on three-dimensional shock control bumps-Reference-Cited by-同舟云学术

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Vortical structures on three-dimensional shock control bumps

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Colliss Simon¹,Babinsky Holger¹,Nubler Klemens,Lutz Thorsten

Affiliation:

1. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-403

Reference27 articles.

1. 4Ogawa, H., Experimental and analytical investigation of transonic shock-wave/boundary-layer interaction control with three-dimensional bumps, PhD thesis,University of Cambridge, 2006.

2. Shock-Wave/Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings

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