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The influence of a compressible boundary on the propagation of gaseous detonations

dc.contributor.authorDabora, Eliahou K. (Eliahou Khedhoory)en_US
dc.date.accessioned2006-02-03T19:18:24Z
dc.date.available2006-02-03T19:18:24Z
dc.date.issued1963en_US
dc.identifierUMR0606en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/4468
dc.format.extent153 bytes
dc.format.extent164392 bytes
dc.format.extent3366 bytes
dc.format.extent206134 bytes
dc.format.extent18175463 bytes
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.subjectDetonation waves.en_US
dc.subjectRocket engines -- Combustion.en_US
dc.titleThe influence of a compressible boundary on the propagation of gaseous detonationsen_US
dc.typeTechnical Reporten_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/4468/5/bab3517.0001.001.pdfen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/4468/4/bab3517.0001.001.txten_US
dc.owningcollnameEngineering, College of - Technical Reports


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