Predictions for the Heat Transfer and Boundary Layer Growth in the Radiatively Driven Hypersonic Wind Tunnel and Comparisons with Experiment at Ultra High Reynolds Number (Invited)-Reference-Cited by-同舟云学术

Predictions for the Heat Transfer and Boundary Layer Growth in the Radiatively Driven Hypersonic Wind Tunnel and Comparisons with Experiment at Ultra High Reynolds Number (Invited)

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
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Author:

Brown Garry¹,Girgis Ihab¹,Miles Richard¹

Affiliation:

1. Princeton University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3128

Reference9 articles.

1. I.G. Girgis, G. L. Brown, R.B. Miles, R. J. Lipinski, "Heat Transfer and Boundary Layer Growth for Ultra High-Reynolds-number Turbulent Boundary Layers for a Radiatively Driven HypersonicWind Tunnel," AIAAPaper 2002-0575

2. I.G. Girgis, G. L. Brown, and R.B. Miles, R. J. Lipinski, "Inviscid and Viscous Predictions for an Ebeam Heated Hypersonic Wind-Tunnel" AIAA Paper 2002-3129 (Invited)

3. L. Martinelli and A. Jameson, " Validation of Multigrid Method for Reynolds Averaged Equations" AIAApaper 88-0414

4. A. Jameson, " Essential Elements of Computational Algorithms for Aerodynamic Analysisand Design", NASACR-97-206268

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