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dc.contributor.advisorNeumann, Ernest P.
dc.contributor.authorHennessey, Thomas Vincent
dc.contributor.authorDuke, John Morgan, Jr.
dc.contributor.authorHennessey, Thomas Vincenten_US
dc.contributor.authorDuke, John Morganen_US
dc.dateSeptember 1946
dc.date.accessioned2012-03-14T17:52:26Z
dc.date.available2012-03-14T17:52:26Z
dc.date.issued1946-09
dc.date.issued1946
dc.identifier.urihttp://hdl.handle.net/10945/6408
dc.descriptionThis thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.en_US
dc.description.urihttp://www.archive.org/details/experimentalstud00henn
dc.language.isoen_US
dc.language.isoen_USen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsApproved for public release; distribution is unlimiteden_US
dc.subject.lcshAeronauticsen_US
dc.titleAn experimental study of flow in a nozzle designed to provide a parallel jet at supersonic speeden_US
dc.typeThesis
dc.typeThesisen_US
dc.contributor.corporateMassachusetts Institute of Technology
dc.contributor.departmentMechanical Engineering
dc.description.serviceU.S. Navy (U.S.N.) authors.en_US
dc.identifier.oclcocn640229614en_US
etd.thesisdegree.nameM.S.en_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.grantorMassachusetts Institute of Technologyen_US
etd.verifiedyesen_US


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