Dilatation Effect in Relaminarization of an Accelerating Supersonic Turbulent Boundary Layer
Author:
Affiliation:
1. University of Tokyo, Tokyo 113, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055368
Reference23 articles.
1. Future Use of Large Eddy Simulation in Aero‐engines
2. Numerical Simulations of Successive Distortions in Supersonic Turbulent Flow
3. Numerical Investigation of Compressible Turbulent Boundary Layer Over Expansion Corner
4. Turbulent structures in accelerating boundary layers
5. Numerical study of sink-flow boundary layers
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