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dc.contributor.authorSturek, Walter B. (Walter Beynon)en_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-10-06T21:22:06Z
dc.date.available2016-10-06T21:22:06Z
dc.date.issued1961en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104709
dc.descriptionJune 1961en_US
dc.descriptionAlso issued as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1961en_US
dc.descriptionIncludes bibliographical referencesen_US
dc.description.abstractA study is made of the flow pattern resulting from the presence of a temperature wake in a uniform velocity field subjected to various adverse pressure gradients. Dimensionless temperature profiles and velocity profiles are presented. A velocity defect appears in the region of high temperature, and the magnitude of the adverse pressure gradient over the range investigated has no effect on the spreading of the temperature wake. A simple theoretical approach is presented which correlates well with the experimental results. The implications of the experimental results and the theoretical approach are discussed with reference to an axial compressor with a temperature wake in the fluid stream at the inlet.en_US
dc.description.sponsorshipUnder the Sponsorship of: General Electric Company and Westinghouse Electric Corporationen_US
dc.format.extent[39] pages in various pagings (some unnumbered)en_US
dc.publisherCambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1961]en_US
dc.relation.ispartofseriesGTL report #64en_US
dc.subject.lccTJ778.M41 G24 no.64en_US
dc.subject.lcshDiffusersen_US
dc.subject.lcshAir jetsen_US
dc.subject.lcshTemperatureen_US
dc.titleTemperature wake in an adverse pressure gradienten_US
dc.typeTechnical Reporten_US
dc.identifier.oclc14192039en_US


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