Development and Breakdown of Gortler Vortices in High Speed Boundary Layers
Author:
Affiliation:
1. NASA Langley Research Center
2. University of California, Los Angeles
3. National Institute of Aeospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-705
Reference30 articles.
1. Gortler instability and supersonic quiet nozzle design
2. Schneider, S.P. "Design of a Mach-6 Quiet-Flow Wind-Tunnel Nozzle using the e**N Method for Transition Estimation," AIAAPaper1998-0546,1998.
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
4. Choudhari, M. M, Li, F. and Edwards, J. E. "Stability analysis of roughness array wake in a high-speed boundary layer,"AIAAPaper2009-0170,2009.
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