Impulse facility simulation of hypervelocity radiating flows
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MorganEtal2006_Impulse_Facility_Simulation_of_Hypervelocity_Radiating_Flows.pdf. Administrators only | Request a copy from author |
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 | ||
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Item Type: | Chapter in Book, Report or Conference volume (Conference contribution) | ||
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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 | ||
Copyright Statement: | This work is covered by copyright. Unless the document is being made available under a Creative Commons Licence, you must assume that re-use is limited to personal use and that permission from the copyright owner must be obtained for all other uses. If the document is available under a Creative Commons License (or other specified license) then refer to the Licence for details of permitted re-use. It is a condition of access that users recognise and abide by the legal requirements associated with these rights. If you believe that this work infringes copyright please provide details by email to qut.copyright@qut.edu.au | ||
Deposited On: | 22 Apr 2014 03:09 | ||
Last Modified: | 03 Mar 2024 10:56 |
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