Adaptive Turbulent Schmidt number approach for Multi-Scale Simulation of Supersonic Crossflow-Reference-Cited by-同舟云学术

Adaptive Turbulent Schmidt number approach for Multi-Scale Simulation of Supersonic Crossflow

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Computational Fluid Dynamics Conference
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Author:

Hassan Ezeldin¹,Aono Hikaru¹,Shyy Wei²,Boles John³,Davis Douglas⁴

Affiliation:

1. University of Michigan, Ann Arbor

2. Hong Kong University of Science and Technology

3. Taitech, Inc.

4. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3702

Reference39 articles.

1. Numerical study of jet injection into a supersonic crossflow

2. Simulation of Transition with a Two-Equation Turbulence Model

3. Gruber, M. R., Nejad, A S., J. C. Dutton. "An Experimental Investigation of Transverse Injection from Circular and Elliptical NozzlesintosupersonicCrossflow," Wright Lab Technical Report Vol. WL-TR-96-2102,1996.

4. Large structure convection velocity measurements in compressible transverse injection flowfields

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