| タイトル | Shock Tunnel Studies of Scramjet Phenomena 1993 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950018974 |
| 著者（英） | Mee, D.; Tuttle, S.; Simmons, J. M.; Paull, A.; Morgan, R. G.; Porter, L.; Wendt, M.; Stalker, R. J.; Bakos, R. J.; Skinner, K. |
| 著者所属（英） | Queensland Univ. |
| 発行日 | 1995-01-01 |
| 言語 | eng |
| 内容記述 | Reports by the staff of the University of Queensland on various research studies related to the advancement of scramjet technology and hypervelocity pulse test facilities are presented. These reports document the tests conducted in the reflected shock tunnel T4 and supporting research facilities that have been used to study the injection, mixing, and combustion of hydrogen fuel in generic scramjets at flow conditions typical of hypersonic flight. In addition, topics include the development of instrumentation and measurement technology, such as combustor wall shear and stream composition in pulse facilities, and numerical studies and analyses of the scramjet combustor process and the test facility operation. This research activity is Supplement 10 under NASA Grant NAGw-674. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 95N25394
NASA-CR-195038
NAS 1.26:195038 |
| 権利 | No Copyright |
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