Validation of a Wall-Layer Model for a Shock-Wave/Boundary-Layer Interaction-Reference-Cited by-同舟云学术

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Validation of a Wall-Layer Model for a Shock-Wave/Boundary-Layer Interaction

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Bond Ryan¹,Blottner Frederick¹,Smith Thomas¹

Affiliation:

1. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-115

Reference19 articles.

1. Implementation and Testing of a Compressible Wall-Layer Model on a Flat Plate

2. A Compressible Wall-Layer Approach Compatible with Various Turbulence Models

3. 5Gant, S. E. "Development and Application of a New Wall Function for Complex Turbulent Flows," Ph.D. thesis,University of Manchester Institute of Science and Technology, Manchester, UK, 2002.

Cited by 1 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. Derivation, implementation, and initial testing of a compressible wall-layer model;International Journal for Numerical Methods in Fluids;2010-03-17

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