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Diagnostic modelling of an expansion tube operating condition

McGilvray, M. and Austin, J. M. and Sharma, M. and Jacobs, P. A. and Morgan, R. G. (2009) Diagnostic modelling of an expansion tube operating condition. Shock Waves, 19 (1). pp. 59-66. ISSN 0938-1287 . https://resolver.caltech.edu/CaltechAUTHORS:20140924-082731206

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Abstract

Computational simulations of an expansion tube were conducted to estimate flow parameters and verify experimental uncertainties. Two types of simulations of the complete facility were undertaken: a one-dimensional simulation, and a hybrid simulation where a one-dimensional simulation of the shock tube section was coupled with a two-dimensional simulation of the acceleration tube. Good agreement between the one-dimensional simulations and experiments were obtained in the shock tube portion of the facility. In the acceleration section, initial two-dimensional simulations did not match the experimentally measured pitot pressure and showed a discrepancy in the shock speed. Further studies examined how the accelerator gas composition affected shock speed, static pressure and pitot pressure levels in expansion tube operation. Subsequent two-dimensional simulations, using an 8% level of air contamination in helium, showed reasonable agreement with experimental data. This prediction of air contamination was later confirmed with experimental measurements of the air partial pressure before operation.


Item Type:Article
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.1007/s00193-009-0187-9 DOIArticle
http://link.springer.com/article/10.1007%2Fs00193-009-0187-9PublisherArticle
Additional Information:© 2009 Springer-Verlag. Received: 23 June 2008; Revised: 17 December 2008; Accepted: 29 January 2009; Published online: 17 February 2009. The authors would like to acknowledge the University of Queensland’s graduate research office for financial support in the form of a Graduate Research Student Travel Award for Matthew McGilvray to visit the University of Illinois. All the simulations detailed in this paperwere undertaken on the Blackhole cluster computer located at the Centre for Hypersonics, University of Queensland. Financial support for the cluster computer was provided by SUN Microsystems and by the Queensland State government under the Smart State program. We thank Rowan Gollan, Carolyn Jacobs, Daniel Potter and Marlies Hankel for running the University of Queensland cluster computer. Experimental work was supported in part by the AFOSR/MURI Grant FA9550-04-1-0425 with Dr. John Schmisseur as program manager.
Group:GALCIT
Funders:
Funding AgencyGrant Number
University of QueenslandUNSPECIFIED
Air Force Office of Scientific Research (AFOSR) Multidisciplinary University Research Initiative (MURI)FA9550-04-1-0425
Subject Keywords:Hypersonic; Ground testing; Expansion tube
Issue or Number:1
Classification Code:PACS: 47.40.Ki · 47.11.−j
Record Number:CaltechAUTHORS:20140924-082731206
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20140924-082731206
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:49972
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:29 Sep 2014 23:03
Last Modified:03 Oct 2019 07:18

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