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dc.contributor.authorBates, Stephen Cuyleren_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-09-27T19:59:03Z
dc.date.available2016-09-27T19:59:03Z
dc.date.issued1977en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104413
dc.descriptionJune 1977en_US
dc.descriptionOriginally presented as the author's thesis, (Sc. D.)--in the M.I.T. Dept. of Aeronautics and Astronautics, 1977en_US
dc.descriptionIncludes bibliographical references (pages 123-124)en_US
dc.description.abstractThe purpose of this work is to contribute to the fundamental understanding of fluid turbulence by visualizing its detailed flow structures. Examination of these coherent structures gives information about the turbulent flow that cannot be deduced from its statistics. This information should reduce the role of empiricism in the analysis of turbulence. The experimental method chosen is to visualize a turbulent plane free shear layer using stop-action photography of a phosphorescing trace gas. Choice of 1) direct photo-excitation, 2) collisional excitation, or 3) collisional de-excitation of the phosphorescencing gas with a planar light beam, permits identification of the emission with a cross-sectional map of the material from one stream that is 1) throughout the flow, 2) molecularly mixed with material from the other free stream (alone), or 3) molecularly unmixed. The plane shear layer visualized has been specified experimentally. Extant requirements for self-preservation are insufficient in general, and make the claim of self-preservation for the experimental flow only probable and not definite. A large data set using all three variations of the visualization technique show structures that imply a large amount of new information about turbulent mixing and turbulent processes. The data shows the structures to be simply connected, with slow variation out of the mean flow plane. Specifically, there is a simply connected region of mixed fluid that always separates material entering the layer from the free streams. Collisional excitation and quenching data strongly imply a turbulent mixing process of random bursting from the free stream, followed by internal viscous decay. The complementary process of turbulent entrainment is recorded in the quenching photos as nibbling of the free stream by the layer, together with a randomly occurring large local amplification of this nibbling, previously thought to be engulfment by the boundary.en_US
dc.description.sponsorshipResearch supported by Pratt & Whitney Aircraft Division, United Technologies Corporation (formerly United Aircraft Corporation)en_US
dc.format.extent124 pagesen_US
dc.publisherCambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine Laboratory, [1977]en_US
dc.relation.ispartofseriesGTL report #134en_US
dc.subject.lccTJ778.M41 G24 no.134en_US
dc.subject.lcshTurbulenceen_US
dc.subject.lcshFlow visualizationen_US
dc.subject.lcshCollisional excitationen_US
dc.subject.lcshPhotography -- Scientific applicationsen_US
dc.titleLuminescent visualization of molecular and turbulent transport in a plane shear layeren_US
dc.typeTechnical Reporten_US
dc.identifier.oclc04231956en_US


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