Numerical Investigations on the Effects of the Declining Back-Edge of MVG
Author:
Affiliation:
1. University of Texas, Arlington
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-714
Reference12 articles.
1. 1P. R. Ashill, J. L. Fulker and K. C. Hackett, "Research at DERA on Sub Boundary Layer Vortex Generators (SBVGs) ," AIAA Paper2001-0887.
2. 3B. H. Anderson, J. Tinapple and L. Surber, "Optimal Control of Shock Wave Turbulent BoundaryLayer Interaction Using Micro-ArrayActuation,"AIAA2006-3197.
3. Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions
4. 5S. Lee and E. Loth, "Supersonic Boundary Layer Interactions with Various Micro-Vortex Generator Geometries," AIAA Paper 2009-3712.
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