Hot-wall reentry testing in hypersonic impulse facilities
Article
Article Title | Hot-wall reentry testing in hypersonic impulse facilities |
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ERA Journal ID | 3575 |
Article Category | Article |
Authors | Zander, F. (Author), Morgan, R. G. (Author), Sheikh, U. (Author), Buttsworth, D. R. (Author) and Teakle, P. R. (Author) |
Journal Title | AIAA Journal: devoted to aerospace research and development |
Journal Citation | 51 (2), pp. 476-484 |
Number of Pages | 8 |
Year | 2013 |
Publisher | American Institute of Aeronautics and Astronautics |
Place of Publication | Reston, VA. United States |
ISSN | 0001-1452 |
1533-385X | |
Digital Object Identifier (DOI) | https://doi.org/10.2514/1.J051867 |
Web Address (URL) | http://arc.aiaa.org/doi/10.2514/1.J051867 |
Abstract | Hypersonic testing in impulse facilities replicates various flow characteristics accurately; however, because of the short test times, some phenomena cannot be fully simulated. Previous testing has been conducted with preheated walls up to 800 K; however, this falls well short of the typical temperatures characteristic of ablators in hypervelocity |
Keywords | flight vehicles; flow characteristics; hypervelocity flow; resistive heating; thermal protection system; ultraviolet spectrometry; wall temperatures |
ANZSRC Field of Research 2020 | 401213. Turbulent flows |
400107. Satellite, space vehicle and missile design and testing | |
400106. Hypersonic propulsion and hypersonic aerothermodynamics | |
Public Notes | © 2012 by Fabian Zander. Permanent restricted access to published version due to publisher copyright policy. |
Byline Affiliations | University of Queensland |
Computational Engineering and Science Research Centre | |
Teakle Composites, Australia | |
Institution of Origin | University of Southern Queensland |
https://research.usq.edu.au/item/q2ww6/hot-wall-reentry-testing-in-hypersonic-impulse-facilities
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