Impulse facility simulation of hypervelocity radiating flows

Morgan, R., McIntyre, Tim, Jacobs, Peter, Buttsworth, David, Macrossan, Michael, Gollan, Rowan, , Brandis, Aaron, Potter, Daniel, Eichmann, Troy, Jacobs, Carolyn, McGilvray, Matt, van Diem, Dwight, & Scott, Michael (2006) Impulse facility simulation of hypervelocity radiating flows. In Wilson, A (Ed.) Proceedings of the 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry [SP-629]. European Space Agency (ESA) Publications Division, The Netherlands, pp. 1-6.

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Description

We describe the X-series impulse facilities at The University of Queensland and show that they can produce useful high speed flows of relevance to the study of high temperature radiating flow flields characteristic of atmospheric entry. Two modes of operation are discussed: (a) the expansion tube mode which is useful for subscale aerodynamic testing of vehicles and (b) the non-reflected shock tube mode which can be used to emulate the nonequilibrium radiating region immediately following the bow shock of a flight vehicle.

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ID Code: 70324
Item Type: Chapter in Book, Report or Conference volume (Conference contribution)
ORCID iD:
Capra, Biancaorcid.org/0000-0002-2540-4728
Measurements or Duration: 6 pages
Keywords: expansion tube, nonreflected-shock tube
ISBN: 92-9092-940-5
Pure ID: 33833679
Divisions: Past > QUT Faculties & Divisions > Science & Engineering Faculty
Copyright Owner: Copyright 2006 European Space Agency
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Deposited On: 22 Apr 2014 03:09
Last Modified: 03 Mar 2024 10:56