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A Computationally Efficient Approach to Hypersonic Reacting Flows

Rabinovitch, J. and Blanquart, G. (2015) A Computationally Efficient Approach to Hypersonic Reacting Flows. In: 29th International Symposium on Shock Waves. Vol.1. Springer , Cham, pp. 173-178. ISBN 978-3-319-16835-7. https://resolver.caltech.edu/CaltechAUTHORS:20170621-102011434

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Abstract

Reproducing hypersonic flight conditions in ground based facilities is a very challenging problem due to the high enthalpies required in the test gas, while simultaneously trying to match the post shock gas composition seen in flight. Experimental facilities have made significant progress in reproducing accurately hypersonic flows, but these facilities generally face issues associated with high operating costs and relatively short and noisy test times. This necessitates the need for high fidelity numerical simulations to aid with the investigation of these flows.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://dx.doi.org/10.1007/978-3-319-16835-7_25DOIArticle
http://rdcu.be/tB3yPublisherFree ReadCube access
ORCID:
AuthorORCID
Rabinovitch, J.0000-0002-1914-7964
Blanquart, G.0000-0002-5074-9728
Additional Information:© 2015 Springer International Publishing Switzerland.
Group:GALCIT
Record Number:CaltechAUTHORS:20170621-102011434
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20170621-102011434
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:78406
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:21 Jun 2017 17:38
Last Modified:29 Apr 2020 19:43

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