Impulse facility simulation of hypervelocity radiating flows
Paper
Morgan, R. G., McIntyre, T. J., Jacobs, P. A., Buttsworth, D. R., Macrossan, M. N., Gollan, R. J., Capra, B. R., Brandis, A. M., Potter, D., Eichmann, T., Jacobs, C. M., McGilvray, M., van Diem, D. and Scott, M. P.. 2006. "Impulse facility simulation of hypervelocity radiating flows." 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry. Rome, Italy 06 - 08 Sep 2006 Noordwijk, Netherlands.
Paper/Presentation Title | Impulse facility simulation of hypervelocity radiating flows |
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Presentation Type | Paper |
Authors | Morgan, R. G. (Author), McIntyre, T. J. (Author), Jacobs, P. A. (Author), Buttsworth, D. R. (Author), Macrossan, M. N. (Author), Gollan, R. J. (Author), Capra, B. R. (Author), Brandis, A. M. (Author), Potter, D. (Author), Eichmann, T. (Author), Jacobs, C. M. (Author), McGilvray, M. (Author), van Diem, D. (Author) and Scott, M. P. (Author) |
Journal or Proceedings Title | European Space Agency (Special Publication) |
Journal Citation | 629, pp. 1-6 |
Number of Pages | 6 |
Year | 2006 |
Place of Publication | Noordwijk, Netherlands |
ISBN | 9789290929406 |
Conference/Event | 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry |
Event Details | 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry Parent International Workshop Radiation of High Temperature Gases in Atmospheric Entry Event Date 06 to end of 08 Sep 2006 Event Location Rome, Italy |
Abstract | 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. |
Keywords | hypervelocity radiating flows; atmospheric entry; aerodynamic testing; spacecraft; atmospheric radiation |
ANZSRC Field of Research 2020 | 400199. Aerospace engineering not elsewhere classified |
401213. Turbulent flows | |
400101. Aerospace materials | |
Public Notes | No evidence of copyright restrictions. |
Byline Affiliations | University of Queensland |
Computational Engineering and Science Research Centre |
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https://research.usq.edu.au/item/9y185/impulse-facility-simulation-of-hypervelocity-radiating-flows
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