Show simple item record

dc.contributor.advisorVavra, M. H.
dc.contributor.authorCommons, Patrick Michael
dc.dateSeptember 1967
dc.date.accessioned2012-08-29T23:32:12Z
dc.date.available2012-08-29T23:32:12Z
dc.date.issued1967-09
dc.identifier.urihttp://hdl.handle.net/10945/12356
dc.descriptionApproved for public release, distribution is unlimiteden_US
dc.description.abstractThe primary purpose of the Transonic Turbine Test Rig is to study the effects of axial and radial clearances on turbine performance. Additionally, the installation was designed to permit the determination of stator discharge velocities by the application of the momentum and moment of momentum equations. Previous attempts to obtain stator discharge velocities by these methods have been unsuccessful. However, during this series of tests, with over 150 hours of useful operating time, the instrumentation and the data acquisition procedures were improved to the extent that the difference between stator discharge velocities obtained from a momentum analysis and those obtained from continuity were reduced to less than three percent.en_US
dc.description.urihttp://www.archive.org/details/instrumentationo00comm
dc.language.isoen_US
dc.publisherMonterey, California. U.S. 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.subject.lcshAeronauticsen_US
dc.titleInstrumentation of the Transonic Turbine Test Rig to determine the performance of turbine inlet guide vanes by the application of the momentum and moment of momentum equationsen_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School
dc.contributor.departmentDepartment of Aeronautics
dc.subject.authorTurbine instrumentationen_US
dc.subject.authorTurbine test rigen_US
dc.subject.authorInlet guide vanesen_US
dc.subject.authorMomentum equationen_US
dc.subject.authorMoment of momentum equationen_US
dc.description.serviceLieutenant, United States Navyen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record