Prediction of heat transfer into a thermally compliant surface in a Mach 5.73 boundary layer using direct numerical simulation-Reference-Cited by-同舟云学术

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Prediction of heat transfer into a thermally compliant surface in a Mach 5.73 boundary layer using direct numerical simulation

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:41st AIAA Fluid Dynamics Conference and Exhibit
language:
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Author:

Ostoich Chrisopher¹,Bodony Daniel¹,Geubelle Philippe¹

Affiliation:

1. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3706

Reference49 articles.

1. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels

2. 2Pozefsky, P., Blevins, R. D., and Laganelli, A. L. "Thermo-vibro-acoustic loads and fatigue of hypersonic flight vehicle structure," Tech. Rep. AFWAL-TR-89-3014, Flight Dynamics Laboratory, AFRL, 1989.

3. On Structural Fatigue Under Random Loading

4. An approximate method for sonic fatigue analysis of plates and shells

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