The Effect of Tunnel Size on Incident Shock Boundary Layer Interaction Experiments-Reference-Cited by-同舟云学术

The Effect of Tunnel Size on Incident Shock Boundary Layer Interaction Experiments

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:

Benek John¹,Suchyta Casimir²,Babinsky Holger³

Affiliation:

1. Air Force Research Laboratory

2. Ohio Aerospace Institute

3. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-862

Reference10 articles.

1. Shock Wave/Turbulent Boundary-Layer Interactions in Rectangular Channels

2. UnsteadyEffectsofShockwaveInducedSeparation,Doerffer,P.,Hirsch,C.,Dussauge,J.P.,andBabinsky,H.eds. NotesonNumericalFluidMechanicsandMultidisciplinaryDesign,Vol.114,Springer-Verlag,Berlin,2010.

3. Delery,J.andMarvin,J.G.`SweptShock-waveboundary-layerinteractions,"AGARD-AG280,February,1966.

4. Settles,G.S.andDolling,D.S."Sweptshock/boundary-layerinteractions-Tutorialandupdate,"AIAAPaper90 -0375,January1990.

5. ShockWaveBoundary-LayerInteractions,Babinsky,H.and Harvey,J.H.,CambridgeUniversityPress,Cambridge, 2011.

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