Coupled fluid/thermal prediction of ablating hypersonic vehicles-Reference-Cited by-同舟云学术

Coupled fluid/thermal prediction of ablating hypersonic vehicles

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Hassan Basil¹,Kuntz David¹,Potter Donald¹

Affiliation:

1. Sandia National Labs., Albuquerque, NM

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-168

Reference70 articles.

1. Kendall, R. M., Bartlett, E. P., Rindall, R. A., and Moyer, C. B. "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator. Part I: Summary Report,"NASA CR-1060, June 1968.

2. Bartlett, E. P., and Kendall, R. M. "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator. Part III: Nonsimilar Solution of the Multicomponent Laminar Boundary Layer by an Integral Matrix Method,"NASA CR-1062,June 1968.

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