Large-Eddy Simulation of Transitional Boundary Layer with Impinging Shock Wave
Author:
Affiliation:
1. University of Tokyo, Tokyo 113-8656, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.16140
Reference27 articles.
1. The 1991 IGTI Scholar Lecture: The Role of Laminar-Turbulent Transition in Gas Turbine Engines
2. Accurate Numerical Simulation of Compressible Transitional Flows in Turbomachinery
3. Shock-boundary layer interaction and transition modelling in turbomachinery flows
4. Boundary layer investigations on a highly loaded transonic compressor cascade with shock/laminar boundary layer interactions
5. Large Eddy Simulation of Shock/Boundary-Layer Interaction
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