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Performance of an aero-space plane propulsion nozzle /Bae, Yoon-Yeong, January 1989 (has links)
Thesis (Ph. D.)--University of Oklahoma, 1989. / Includes bibliographical references (leaves 54-56).
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Experimental analysis of plug nozzlesBalasaygun, Eray, 1941- January 1964 (has links)
No description available.
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Parametric considerations in the design and performance of a fluidic direct impact modulatorMcgregor, Ronald Wayne 12 1900 (has links)
No description available.
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Experimental determination of three-dimensional liquid rocket nozzle admittancesBell, William Alvin 08 1900 (has links)
No description available.
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The effect of nozzle nonlinearities on the nonlinear stability of liquid rocket motorsPadmanabhan, Mysore Srikantiah 12 1900 (has links)
No description available.
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Development of an experimental method for the determination of local heat flux in small diameter, cooled nozzlesKunz, Eric Gibson 12 1900 (has links)
No description available.
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Inclusion behaviour in steel flows through convergent nozzlesDuncombe, John Trevor January 1989 (has links)
It is well established that nozzle blockage in Al-killed continuously cast steels is caused by the deposition of preexisting Al 0 inclusions at the narrowest part of the nozzle. Thisa adhere strongly at the wall by interfacial forces. The theory examined in this thesis is that during the curved flow path through the nozzle, inclusions move towards the nozzle wall by the action of centripetal force. A mathematical model has been developed which takes account of centripetal, gravitational, and drag forces. A computer programme has been written to predict particle behaviour in nozzle flows. To study the behaviour of second phase particles, a water model using a perspex tundish and an interchangeable glass nozzle has been built. Turbulence has been almost completely removed from the experimental tundish. Hydrogen bubbles electrolytically generated in water have been used to simulate the inclusions in steel and their flow paths through the nozzle have been recorded by cine photography. With frame by frame analysis of the films, the effects of bubble size, (50 pm to 1000 um), and flow velocity have been studied. Two experimental nozzles have been tested which have demonstrated the importance of limiting the centripetal force. It has been shown that there is a good relationship between hydrogen bubble behaviour and model predictions. This has been particularly true of small bubbles near the nozzle wall. By comparing the results with other experimental work it has been shown that centripetal forces can have a significant effect on the rate of blocking. Practical suggestions for reducing the turbulent behaviour in steel tundishes and nozzles are made. The merits of an improved nozzle design which takes advantage of the results of the model work are discussed.
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A model for the prediction of critical flow rates in two-phase bubbly mixtures /Zavodny, Eugene Nance. January 1971 (has links)
Thesis (Ph.D.)--University of Tulsa, 1971. / Bibliography: leaves 95-100.
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The evolution of the near field of a precessing jet flowClayfield, Kimberley Christina. January 2004 (has links)
Thesis (Ph.D.)--University of Adelaide, School of Mechanical Engineering, 2005. / Title from title page of source document; viewed 19 July 2005. Bibliography: p. 213-224 of source document. Also available in print.
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A study of nozzle jet application to winter maintenance vehiclesHu, Xiaowei. January 2007 (has links)
Thesis (M.S.)--University of Nevada, Reno, 2007. / "December, 2007." Includes bibliographical references (leaves 60-65). Online version available on the World Wide Web.
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