Normal Shock Boundary Layer Interaction Control Using Micro-Vortex Generators-Reference-Cited by-同舟云学术

Normal Shock Boundary Layer Interaction Control Using Micro-Vortex Generators

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:5th Flow Control Conference
language:
Short-container-title:

Author:

Lee Sang¹,Loth Eric²,Babinsky Holger³

Affiliation:

1. University of Illinois, Urbana-Champaign

2. University of Virginia

3. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4254

Reference28 articles.

1. 1Loth,E,"SmartMesoflapsforControlofShockBoundaryLayerInteractions",AIAA2000-2476

2. Adaptive wing and flow control technology

3. 3Holmes, A. E., Hickey, P. K., Murphy, W. R., Hilton, D. A. "The Application of Sub-Boundary Layer Vortex Generators toReduce Canopy Mach Rumble InteriorNoise on the GulfstreamIII",AIAA87-0084

4. 4Ashill, P., Fulker, J. and Hackett, K. "Research at DERA on Sub-Boundary Layer Vortex Generators (SBVGs)", AIAA 2001-0831

5. Effect of Microvortex Generators On Seperated Normal Shock/ Boundary Layer Interactions

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