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Stationary and rotating hot jet ignition and flame propagation in a premixed cell /Bilgin, Murat. January 1998 (has links)
Thesis (Ph. D.)--University of Washington, 1998. / Vita. Includes bibliographical references (leaves [198]-190).
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The enhanced mixing burner / submitted by Graham Jerrold Nathan for the Degree of Doctor of PhilosophyNathan, Graham Jerrold, University of Adelaide. Dept. of Mechanical Engineering January 1988 (has links)
Cased / Bibliography: p. 210-219 / xx, 239 leaves : ill. (some col.) ; 30 cm. + 1 16mm film / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / Thesis (Ph.D.)--University of Adelaide, Dept. of Mechanical Engineering, 1989
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Under-expanding sonic jet discharging from a cylindrical concave wallElabdin, Mohamed Nabil Mohamed Zein. January 1975 (has links)
No description available.
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Under-expanding sonic jet discharging from a cylindrical concave wallElabdin, Mohamed Nabil Mohamed Zein. January 1975 (has links)
No description available.
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An evaluation of nozzle response to transient disturbancesAggarwal, Suresh Kumar 05 1900 (has links)
No description available.
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Characterization of the near-field flow structure of an acoustically self-excited jet in a large enclosure using particle image velocimetry (PIV) /Tobias, Jason A. January 1900 (has links)
Thesis (M.S.)--Oregon State University, 2008. / Printout. Includes bibliographical references (leaves 72-74). Also available on the World Wide Web.
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An Investigative Design of Gas Jet Nozzles and their Flow Field Effect on Spatial DistributionPhengsomphone, Adam 01 January 2022 (has links)
Within this study, the presented material has the objective of providing insight and design characteristics for gas jet nozzles that experimentalists and researchers should consider when utilizing this experimental method. Firstly, this study introduces the developing history and necessity for gas jet experiments and its well-known drawbacks, eventually leading to recent studies and founded knowledge regarding the nozzle geometry dependence on the flow field. The simulation methodology of this study will be presented where the discretization of the computational domain, selection of the flow physics model, and overall design of the nozzle geometry is explained and justified. The flow field data from these simulations will then be presented and compared against various analytical relations taken from literature to analyze differences among the different datasets. Finally, interpretation and discussion of the results will lead to design recommendations, reasoning, and optimization of gas jet nozzles that experimentalists should consider when deciding to incorporate the gas jet nozzle within their experiments.
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Fluid dynamic means of varying the thrust vector from an axisymmetric nozzle / submitted by Steven Slavko Vidakovic.Vidakovic, Steven Slavko January 1995 (has links)
Bibliography: leaves 190-212. / xxiii, 240 leaves : ill. ; 30 cm. / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / This thesis describes a thrust vectoring nozzle (TVN) which produces a jet which may be deflected at angles in excess of 80o from the nozzle axis by fluid dynamic means, while maintaining total thrust efficiency of the order of 50%, or at 50o with an efficiency of the order of 70%. The thrust vectoring by fluid dynamic means is achieved by injecting secondary fluid at the nozzle throat and partially separating the primary jet causing it to deform. / Thesis (Ph.D.)--University of Adelaide, Dept. of Mechanical Engineering, 1995
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Joining of aluminum and long fiber thermoplastic (LFT) compositesKulkarni, Rahul R. January 2007 (has links) (PDF)
Thesis (Ph. D.)--University of Alabama at Birmingham, 2007. / Additional advisors: Derrick R. Dean, Alan W. Eberhardt, Ramana G. Reddy, Uday K. Vaidya. Description based on contents viewed Feb. 13, 2009; title from PDF t.p. Includes bibliographical references.
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A method for propulsion nozzle designEskandarian, Azim January 1983 (has links)
An inverse method for the design of exhaust nozzles with a specified transonic pressure distribution is presented. A problem of mixed Neumann and Dirichlet boundary condition is solved. A successive line relaxation process is used to solve the array of velocity potentials in the entire flow field. The streamlines are then displaced to produce boundaries which match a desired pressure distribution. Various cases are tested to verify the reliability of the method. The design calculation proves to be efficient and accurate. / M.S.
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