Implementation and Testing of a Compressible Wall-Layer Model on a Flat Plate-Reference-Cited by-同舟云学术

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

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Bond Ryan¹,Blottner Frederick¹

Affiliation:

1. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1331

Reference34 articles.

1. On the use of wall functions as boundary conditions for two-dimensional separated compressible flows

2. Assessment of One- and Two-Equation Turbulence Models for Hypersonic Transitional Flows

3. Methodology for Turbulence Model Validation: Application to Hypersonic Flows

4. Review and assessment of turbulence models for hypersonic flows

5. Wall matching, a rational alternative to wall functions

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. Validation of a Wall-Layer Model for a Shock-Wave/Boundary-Layer Interaction;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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