Numerical Simulations of the University of Michigan Shock Boundary-Layer Interaction Experiments-Reference-Cited by-同舟云学术

Numerical Simulations of the University of Michigan Shock Boundary-Layer Interaction Experiments

Published:2015-05 Issue:5 Volume:53 Page:1134-1145
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Friedlander David J.,Georgiadis Nicholas J.,Turner Mark G.,Orkwis Paul D.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053040

Reference21 articles.

1. Numerical Prediction of Supersonic Shock-Boundary Layer Interaction

2. RumseyC. L. “CFL3D Contribution to the AIAA Supersonic Shock Boundary Layer Interaction Workshop,” NASA TM 2010-216858, Oct. 2010.

3. GeorgiadisN. J.VyasM. A.YoderD. A. “Wind-US Code Contribution to the First AIAA Shock Boundary Layer Interaction Prediction Workshop,” NASA TM 2013-217837, Feb. 2013.

4. Investigation by Particle Image Velocimetry Measurements of Oblique Shock Reflection with Separation

5. Stereo particle image velocimetry of nonequilibrium turbulence relaxation in a supersonic boundary layer

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