Numerical Computations of Hypersonic Boundary-Layer over Surface Irregularities
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1572
Reference18 articles.
1. Duan, 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. Marxen, O. and Iaccarino, G. "Simulation of the Effect of a Roughness Element on High-speed Boundarylayer Instability," AIAAPaper 2008-4400,2008.
3. Choudhari, M., Li, F., and Edwards, J.E. "Stability Analysis of Roughness Array Wake in a High-Speed BoundaryLayer," AIAAPaper 2009-0170,2009.
4. Choudhari, M. M., Li, F., Wu, M., Chang, C.L., Edwards, J., Kegerise, M., and King, R. "Laminar-Turbulent Transition behind Discrete Roughness Elements in a High-Speed Boundary Layer," AIAA Paper 2010-1575,2010.
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