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Deriving Features of Reacting Hypersonic Flows from Gradients at Curved Shocks

Hornung, H. G. (2008) Deriving Features of Reacting Hypersonic Flows from Gradients at Curved Shocks. In: 5th AIAA Theoretical Fluid Mechanics Conference. American Institute of Aeronautics and Astronautics , Reston, VA, Art. No. 2008-4340. ISBN 978-1-60086-995-2. https://resolver.caltech.edu/CaltechAUTHORS:20200330-080442903

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Abstract

The shock jump relations for gradients of flow variables are presented in the case of a uniform steady free stream with a curved shock that may trigger endothermic or exothermic chemical reaction. The rich information that can be obtained from these is used in order to derive field information for flow variables as well as details about the sonic line. This presentation collects, reviews and extends work that has been published previously in various places. Comparisons with experiment and with numerical computations are given in some cases. The gradient jump relations are Likely to be useful for higher-order numerical schemes that use shock fitting.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/6.2008-4340DOIArticle
ORCID:
AuthorORCID
Hornung, H. G.0000-0002-4903-8419
Additional Information:© 2008 by Hans G. Hornung. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
Group:GALCIT
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2008-4340
Record Number:CaltechAUTHORS:20200330-080442903
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20200330-080442903
Official Citation:Deriving Features of Reacting Hypersonic Flows from Gradients at Curved Shocks. Hans Hornung. 5th AIAA Theoretical Fluid Mechanics Conference. June 2008; doi: 10.2514/6.2008-4340
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:102164
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:30 Mar 2020 15:32
Last Modified:30 Mar 2020 15:32

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