Effects of Cavities and Protuberances on Transition over Hypersonic Vehicles
Author:
Affiliation:
1. NASA Langley Research Center
2. University of Alabama, Birmingham
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3245
Reference28 articles.
1. 1Duan, L., Wang, X., and Zhong, X. "A High-Order Cut-Cell Method for Numerical Simulation of Hypersonic-BoundaryTransition with Surface Roughness," AIAAPaper 2008-3732,2008.
2. 2Marxen, O. and Iaccarino, G. "Simulation of the Effect of a Roughness Element on High-speed Boundarylayer Instability," AIAAPaper 2008-4400,2008.
3. Hypersonic viscous flow over large roughness elements
4. 4Choudhari, M., Li, F., and Edwards, J.E. "Stability Analysis of Roughness Array Wake in a High-Speed BoundaryLayer," AIAAPaper 2009-0170,2009.
5. 5Chang, C.L., Choudhari, M. M., and Li, F. "Numerical Computations of Hypersonic Boundary-Layer over Surface Irregularities," AIAA Paper2010-1572,2010.
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