Overview

Reports by the staff of the University of Queensland on various research studies related to the advancement of scramjet technology 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. Wendt, M. and Nettleton, M. and Morgan, R. G. and Skinner, K. and Casey, R. and Stalker, R. and Brescianini, C. and Paull, A. and Allen, G. and Smart, M. Unspecified Center NASA-CR-191428, NAS 1.26:191428 NAGW-674; RTOP 505-70-62-02...

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9781724372925

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