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dc.contributor.authorPapailiou, Kyriacos D.
dc.date.accessioned2013-01-23T21:56:37Z
dc.date.available2013-01-23T21:56:37Z
dc.date.issued1971-09
dc.identifier.urihttp://hdl.handle.net/10945/26182
dc.description.abstractA computer program is presented to determine the three-dimensional flow conditions in an axial flow compressor stage. Entropy and energy gradients are taken into account as well as the radial shift and the curvatures of the axisymmetric stream surfaces. The program can be used at elevated Mach numbers since shock losses and compressibility effects are included. It represents an extension of work done for a research program to investigate the tip clearance effects in a three-stage compressoren_US
dc.description.urihttp://archive.org/details/programfordesign00papa
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. 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.lcshCompressorsen_US
dc.titleProgram for the design of an axial compressor stage based on the radial equilibrium equationsen_US
dc.typeTechnical Reporten_US
dc.identifier.npsreportNPS57PY71091A


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