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dc.contributor.authorLess, David Matthewen_US
dc.date.accessioned2017-11-09T21:09:06Z
dc.date.available2017-11-09T21:09:06Z
dc.date.issued1982en_US
dc.identifier.urihttp://hdl.handle.net/10919/80133
dc.description.abstractAn experimental study of the transverse injection of a particle laden liquid jet into a supersonic air stream was conducted. Five micron diameter silicon dioxide particles with a specific gravity of 2.35 were suspended in water and injected across a Mach 3.0 air stream. A stagnation pressure of 4.2 atm. and a stagnation temperature of 15° C were maintained throughout the tests. Particle loadings of up to 68% by mass were injected. The penetration and behavior of the jets were examined through a light extinction survey and through a series of streak arid nanoflash photographs. Some of the particles were found to agglomerate into clumps ranging up to 40 microns in diameter. The clumps separated from the liquid plume and penetrated up to 45% further into the air stream than the liquid. For mass loadings greater than 55%, the jet column appeared more rigid than those of lower or zero particle loadings.en
dc.format.extentv, 46, [1] leavesen_US
dc.format.mimetypeapplication/pdfen_US
dc.language.isoen_USen_US
dc.publisherVirginia Polytechnic Institute and State Universityen_US
dc.relation.isformatofOCLC# 8511086
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V855 1982.L477en_US
dc.subject.lcshJets -- Fluid dynamicsen_US
dc.subject.lcshAir flowen_US
dc.subject.lcshTurbulenceen_US
dc.titleTraverse injection of a particle-laden liquid jet into a supersonic air streamen_US
dc.typeThesisen_US
dc.contributor.departmentAerospace and Ocean Engineeringen_US
dc.description.degreeMaster of Scienceen_US
thesis.degree.nameMaster of Scienceen_US
thesis.degree.levelmastersen_US
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen_US
thesis.degree.disciplineAerospace and Ocean Engineeringen_US
dc.type.dcmitypeTexten_US


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