Section 12
You have free access to this content
Investigation of high-speed boundary-layer transition by DNS
Article first published online: 13 DEC 2004
DOI: 10.1002/pamm.200410216
Copyright © 2004 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim
Additional Information
How to Cite
Stemmer, C. and Adams, N. A. (2004), Investigation of high-speed boundary-layer transition by DNS. Proc. Appl. Math. Mech., 4: 470–471. doi: 10.1002/pamm.200410216
Publication History
- Issue published online: 13 DEC 2004
- Article first published online: 13 DEC 2004
References
- [1]and . A High-Resolution Hybrid Compact-ENO Scheme for Shock-Turbulence Interaction Problems. J. Comp. Phys., 127, 27–51, 1996).
- [2], A Review of Reaction Rates in High Temperature Air, AIAA Paper 89-1740, 1989.
- [3]. Flat-Plate Boundary-Layer Hypersonic Transition. Annual Research Briefs 2002. Center for Turbulence Research, Stanford University, NASA Ames, 389–396, 2002.
- [4]. Transition in hypersonic flows including high-temperature gas effects. Annual Research Briefs 2003. Center for Turbulence Research, Stanford University, NASA Ames, 475–479, 2003.
- [5]and . Experimental study of secondary stability in a hypersonic shock layer on a flat plate. J. of Fluid. Mech.. 412, 259–277, 2000).
- [6]and . An experimental study of density waves in a hypersonic shock layer on a flat plate. Phys. of Fluids. 12(6), 1544–1553, 2000).
- [7]. Boundary-Layer Stability Theory, Jet Propulsion Laboratory, Pasadena, USA ,JPL Report 900-277 Rev. A, 1969.
- [8], Flight data for boundary-layer transition at hypersonic and supersonic speeds, J. of Spacecraft and Rockets, 36, 8–20, 1999).
- [9]and , On Hypersonic Boundary-Layer Stability, AIAA Paper 92-0737, 1992.
- [10]and , Unstable branches of a hypersonic, chemically reacting boundary layer, Engineering Turbulence Modeling and Experiments 3, IN: Proceedings of the Boundary Layer Transition and Control Conference organized by The Royal Aeronautical Society, Peterhouse College, Cambridge, UK, 19.1–19.13, April 8-12, 1991.
- [11]and , Real gas effects on hypersonic boundary-layer stability, Phys. Fluids A, 3(5, 803–821, 1991).
- [12]. Direct Numerical Simulation of Turbulent Compression Ramp Flow. Theor. and Comp. Fl. Dynamics, 12, 109–129, 1998).
- [13]. Direct Simulation of the Turbulent Boundary Layer along a compression ramp at M = 3 and Reθ = 1685. J. Fluid Mech., 420, 47–83, 2000).
- [14]. Compact Finite-Difference Schemes With Spectral-Like Resolution, J. Comp. Phys., Vol. 103, 16–42, Academic Press, San Diego, 1992.
- [15]. Chemistry of external flows, Aerothermochemistry for Hypersonic Technology, VKI-LS 1995-04,

1617-7061/asset/2130_left.gif?v=1&s=31d9c7dbbe937e9e4955a0f5ae18213dd9a41f7b)
1617-7061/asset/cover.gif?v=1&s=79b6ccfe3470758033c99b476335ce58b5a38819)