Spelling suggestions: "subject:"heat - atransmission"" "subject:"heat - cotransmission""
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Interferometric studies of laminar and transitional free convection heat transfer in waterMehta, Jayesh Madanlal 08 1900 (has links)
No description available.
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The effects of roughness on heat transfer from open channel flowMoss, Michael David 05 1900 (has links)
No description available.
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Turbulent convection in microchannelsAdams, Thomas M. 12 1900 (has links)
No description available.
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Optimal well location in contaminant plume remediationShea, Charles Brian 12 1900 (has links)
No description available.
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Heat transfer resulting from a turbulent, submerged jet impinging on a phase change materialBhansali, Anil P. 08 1900 (has links)
No description available.
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Optimal well location in contaminant plume containmentRatzlaff, Steven Abraham 05 1900 (has links)
No description available.
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Evaporation from flowing channels under thermal loadingFulford, Janice Marie Canfield 08 1900 (has links)
No description available.
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Flow and heat transfer for impinging round turbulent jetsObot, Nsima Tom. January 1980 (has links)
Characteristics of the flow field and of impingement surface heat transfer for round, turbulent jets were studied experimentally. / The effects on the flow field and heat transfer of nozzle geometry, i.e. nozzle length, l(,n)/d(,n), and nozzle entrance configuration (contoured and sharp-edged), and semi-confinement were investigated. In addition, the role of suction on the development of flow was considered. / Effects of nozzle geometry on the flow field and on heat transfer are to divide the nozzles tested into two groups; the long (10 (LESSTHEQ) l(,n)/d(,n) (LESSTHEQ) 50) nozzles with similar characteristics and modest differences between them, and the short (l(,n)/d(,n) = 1) nozzles with distinctly different patterns for flow and heat transfer. / Semi-confinement restricts interaction and mixing between the jet and the ambient fluid and hence reduces entrainment, and causes significant reductions in local heat transfer coefficients over most of the impingement surface. / In general, application of suction up to V(,w) = 0.25 m/s or 0.42% of the nozzle exit average velocity reduces the boundary layer thickness, increases radial velocities adjacent to the impingement surface, thereby velocity gradients near the wall.
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Heat and mass transfer under a laminar impinging jetLi, Yau-Kun January 1977 (has links)
No description available.
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Flow and heat transfer measurements in a gas turbine wall cooling passageIeronymidis, Ioannis January 2005 (has links)
No description available.
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