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dc.contributor.authorMullan, Philip Josephen_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-10-06T21:21:52Z
dc.date.available2016-10-06T21:21:52Z
dc.date.issued1959en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104672
dc.descriptionMay 1959en_US
dc.descriptionAlso issued as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1959en_US
dc.descriptionIncludes bibliographical references (leaf [18])en_US
dc.description.abstractThe experimental performance of two axial inducers is presented. One of the :designs is analytical and includes radial equilibrium considerations. The other is a simple helix, with a constant pitch angle. The performance data consists of two parts; conventional non-cavitating pump performance, and performance with cavitation. High speed pictures of the cavitation formations were taken.en_US
dc.format.extent17, [1], [51] leavesen_US
dc.publisherCambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959]en_US
dc.relation.ispartofseriesGTL report #53en_US
dc.subject.lccTJ267.A1 M37 no.53en_US
dc.subject.lcshCavitationen_US
dc.subject.lcshTurbomachinesen_US
dc.titleAn investigation of cavitating inducers for turbopumpsen_US
dc.typeTechnical Reporten_US
dc.identifier.oclc09162384en_US


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