Two-component LDV investigation of 3-dimensional shock/turbulent boundary layer interactions
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. California, University,Berkeley
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-553
Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Performance of Turbulence Modeling in Simulation of the HIFiRE-1 Flight Test;Journal of Spacecraft and Rockets;2014-01
2. High-Speed Turbulent Separated Flows: Consistency of Mathematical Models and Flow Physics;AIAA Journal;1998-05
3. Structure of a Supersonic Three-Dimensional Cylinder/Offset-Flare Turbulent Interaction;Journal of Spacecraft and Rockets;1997-05
4. Supersonic compression-corner applications of a multiscale model forturbulent flows;AIAA Journal;1990-07
5. Numerical simulation of a turbulent flow through a shock wave;21st Fluid Dynamics, Plasma Dynamics and Lasers Conference;1990-06-18
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