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Design report of hybrid compressor and associated test rig

dc.contributor.authorVavra, Michael Hans
dc.date1973-07
dc.date.accessioned2013-02-27T23:36:41Z
dc.date.available2013-02-27T23:36:41Z
dc.date.issued1973-07
dc.identifier.urihttps://hdl.handle.net/10945/29245
dc.description.abstractThe report presents the aerodynamic calculations and describes the mechanical features of a test rig that has been designed at the Turbopropulsion Laboratory, Department of Aeronautics, for research work on a special type of centrifugal compressor. This so-called Hybrid compressor consists of a centrifugal rotor with 180 deg flow deflection in the meridional plane followed by an axial flow diffusor. The report establishes a method to predict the off-design performance of the compressor, which can be applied also to conventional centrifugal compressors. Extensive use is made of modern programmable calculators, and programs are presented to show the effectiveness of these tools in engineering endeavors. (Author)en_US
dc.description.sponsorshipNavy Department Naval Air Systems Command, Code 330C AIRTASK No. A3303300/186B/3FU1U32301en_US
dc.description.urihttp://archive.org/details/designreportofhy00vavr
dc.format.extentNAen_US
dc.language.isoen_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. Copyright protection is not available for this work in the United States.en_US
dc.subject.lcshELECTROMAGNETIC THEORY--MATHEMATICAL MODELS.en_US
dc.titleDesign report of hybrid compressor and associated test rigen_US
dc.typeTechnical Reporten_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.description.recognitionNAen_US
dc.identifier.oclcNA
dc.identifier.npsreportNPS-57Va73071A


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