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dc.contributor.advisorVavra, M.H.
dc.contributor.authorRiley, Michael William
dc.date.accessioned2014-09-10T17:01:06Z
dc.date.available2014-09-10T17:01:06Z
dc.date.issued1966-12
dc.identifier.urihttp://hdl.handle.net/10945/43296
dc.descriptionApproved for public release; distribution is unlimiteden_US
dc.description.abstractThis study was conducted to establish the performance parameters of a radial in-flow, dual discharge turbine and to determine the effect of axial clearance on these parameters. The results of the tests can be utilized for design improvements and for predicting off-design operating conditions. The air tests of the turbine were made at several total-to-static pressure ratios. The study presents data obtained from measured rotor discharge flow conditions as well as overall turbine conditions. The test turbine is installed at the Propulsion Laboratory of the Naval Postgraduate School, Monterey, California.en_US
dc.description.urihttp://archive.org/details/theeffectofaxial1094543296
dc.format.extent184 p.en_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.en_US
dc.titleThe Effect of Axial Clearance on the Performance of a Duel Discharge Radial Turbineen_US
dc.typeThesisen_US
dc.contributor.departmentDepartment of Aeronautics
dc.subject.authorRadial Turbineen_US
dc.subject.authorAxial clearanceen_US
dc.subject.authorPerformance parametersen_US
dc.description.serviceUS Navy (USN) authoren_US
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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