Linear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2
Author:
Affiliation:
1. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of Russian Academy of Sciences, Institutskaya Str. 4/1, Novosibirsk 630090, Russia
2. Novosibirsk State University, Novosibirsk 630090, Russia
Funder
Russian Foundation for Basic Research (RFBR)
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4952999
Reference30 articles.
1. D. Arnal, “Boundary layer transition: Predictions based on linear theory,” Progress in Transition Modeling, AGARD Report 793, 1994.
2. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability
3. The Origin of Turbulence in Near-Wall Flows
4. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS
5. Crossflow disturbances in three-dimensional boundary layers: nonlinear development, wave interaction and secondary instability
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