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Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows

Rabinovitch, Jason and Blanquart, Guillaume (2017) Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows. Journal of Propulsion and Power, 33 (3). pp. 776-792. ISSN 0748-4658. https://resolver.caltech.edu/CaltechAUTHORS:20190211-103624005

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Abstract

The performance of different constraints for the rate-controlled constrained-equilibrium (RCCE) method is investigated in the context of modeling reacting flows characteristic of hypervelocity ground testing facilities and reentry conditions. Although the RCCE approach has been used widely in the past, its application in non-combustion-based reacting flows is rarely done; the flows being investigated in this work do not contain species that can easily be classified as reactants and/or products. The effectiveness of different constraints is investigated before running a full computational simulation, and new constraints not reported in the existing literature are introduced. A constraint based on the enthalpy of formation is shown to work well for the two gas models used for flows that involve both shocks and steady expansions.


Item Type:Article
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/1.B36226DOIArticle
ORCID:
AuthorORCID
Rabinovitch, Jason0000-0002-1914-7964
Blanquart, Guillaume0000-0002-5074-9728
Additional Information:© 2016 by Jason Rabinovitch. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Received 25 February 2016; revision received 21 August 2016; accepted for publication 22 August 2016; published online 14 November 2016. Funding for this work was provided by the U.S. Air Force Office of Scientific Research, Grant FA9550-12-1-0472.
Group:GALCIT
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)FA9550-12-1-0472
Issue or Number:3
Record Number:CaltechAUTHORS:20190211-103624005
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20190211-103624005
Official Citation:Rate-Controlled Constrained Equilibrium for Nozzle and Shock Flows Jason Rabinovitch and Guillaume Blanquart Journal of Propulsion and Power 2017 33:3, 776-792; doi: 10.2514/1.B36226
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:92831
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:12 Feb 2019 22:15
Last Modified:03 Oct 2019 20:48

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