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dc.contributor.authorKumar, Ajayen_US
dc.contributor.authorKerrebrock, Jack L.en_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-10-06T21:22:02Z
dc.date.available2016-10-06T21:22:02Z
dc.date.issued1971en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104696
dc.descriptionFebruary 1971en_US
dc.descriptionIncludes bibliographical references (leaf 12)en_US
dc.description.abstractThe mechanism of rotor wake interaction with stators has been examined experimentally by using helium, injected into the rotor wakes, as a tracer for the wake fluid. Time averaged helium Drofiles downstream of the stator, measured with a thermal conductivity cell, indicate the time averaged distribution of rotor wake fluid at the stator exit. The results are in qualitative agreement with the wake transport theory of Kerrebrock and Mikolajczak, but indicate the need for accounting for differential radial drifts of the wake fluid which encounters the motion and pressure sides of the stator blades. They also indicate that the wake transport theory is valid only when the stators flow is not separated.en_US
dc.description.sponsorshipThis Research Carried Out in the Gas Turbine Laboratory, M.I.T., Supported in Part by Pratt & Whitney Aircraft, Division of United Aircraft Corporation, and in Part by the General Electric Companyen_US
dc.format.extent12 leavesen_US
dc.publisherCambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1971]en_US
dc.relation.ispartofseriesGTL report #103en_US
dc.subject.lccTJ778.M41 G24 no.103en_US
dc.subject.lcshWakes (Fluid dynamics)en_US
dc.subject.lcshTurbomachinesen_US
dc.subject.lcshCompressors -- Bladesen_US
dc.titleRotor wake transport in turbomachine statorsen_US
dc.typeTechnical Reporten_US
dc.identifier.oclc09917312en_US


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