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dc.contributor.advisorShreeve, Raymond P.
dc.contributor.authorSherman, Michael H.
dc.date.accessioned2013-01-23T21:55:34Z
dc.date.available2013-01-23T21:55:34Z
dc.date.issued1989
dc.identifier.urihttp://hdl.handle.net/10945/26017
dc.description.urihttp://archive.org/details/investigationint00sher
dc.format.extent139 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.titleAn investigation into the use of an existing shock tube as a driver for a hypersonic shock tunnel.en_US
dc.typeThesisen_US
dc.contributor.corporateNA
dc.contributor.schoolNA
dc.contributor.departmentAeronautical Engineering
dc.description.recognitionNAen_US
dc.identifier.oclcocm82724519
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


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