RANS and Hybrid LES/RANS Simulation of the Effects of Micro Vortex Generators Using Immersed Boundary Methods
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3728
Reference27 articles.
1. 1Délery, J. M. "Shock Wave/Turbulent Boundary Layer Interaction and its Control", Progress in Aerospace Sciences.Vol22,pp209-280,1985.
2. 2Anderson, B. H., Tinapple, J., and Surber, L. "Optimal Control of Shock Wave Turbulent Boundary Layer InteractionsusingMicro-ArrayActuation",June2006,AIAA -2006-3197.
3. 3Holden, H. A., and Babinsky, H. "Vortex Generators Near Shock/ Boundary Layer Interactions", AIAA paper 2004-1242,January,2004.
4. 4Ashill, P. R., Fulker, J. L., and Hackett, K. C. "Research at DERA on Sub Boundary Layer Vortex Generators (SBVGs,AIAApaper2001-0887,Jan.2001.
5. 5Smith, A. N., Holden, H. A., Babinsky, H., Fulker, J. L., and Ashill, P. R. "Control of Normal Shock Wave / TurbulentBoundaryLayerInteractionsUsing Streamwise Grooves",AIAApaper2002-0978, Jan.2002.
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