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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
211

An investigation into the transient response characteristics of an exhaust gas turbocharger

Stockton, E. C. January 1979 (has links)
No description available.
212

The Development of Thermal Recompression Evaporators

Grover, P. D. January 1975 (has links)
No description available.
213

Heat transfer from solid particles to gases in a falling bed contractor

Kumar, V. G. January 1975 (has links)
No description available.
214

Scale and reynolds number effects on some axial flow turbo-machines

Salami, L. A. January 1971 (has links)
No description available.
215

Investigation of the influence of Droplets on the properties of liquid fuel jets

Pauah, V. P. January 1976 (has links)
No description available.
216

The Simulation and Control of Thermal Regenerators

Burns, A. January 1978 (has links)
No description available.
217

Forced convection heat transfer in turbulent pipe flow with variable fluid properties

Ibrahim, M. B. January 1977 (has links)
No description available.
218

Numerical study of simulated low Reynolds number axial turbine blades with flow transition

Kazi, Sheila K. January 2007 (has links)
Two main sources of high losses in small axial turbines are the tip leakage loss and the Reynolds number related loss. The extents of these losses are directly related to blade geometry. Due to limitation in manufacturing capabilities and the prohibitive cost of precision engineering often the manufactured blade is very different from the design or the ideal blade shape and as a result the component efficiency degrades. Reynolds number effect plays a very important role in the low efficiency of small axial turbines. The effect of low Reynolds number is essentially separation of the flow resulting in high losses. Unlike in large turbines, where the Reynolds number is above 10e5, depending on size the Reynolds number over which a small turbine operates can be as low as 10e4. At this range the flow is laminar over a large extent of the blade and is very susceptible to laminar separation resulting in high losses. Since due to the aerodynamics this is inevitable, the only resort for an engineer is to design a blade that will delay separation to a point which will either result in turbulent separation or a transitional-laminar separation resulting in a smaller separation bubble. The design of such blades requires in depth knowledge on the field of flow transitional methods. An existing flow transition model has been implemented with simple modifications for separated flow in an in-house CFD code. Once validated against available experimental data, a parametric study has been conducted, where the effects of Reynolds number, velocity ratio, the turbulence levels and the location of maximum loading has been tested on a simulated turbine flow. Two different velocity distributions were tested. The combined results provided an understanding of the aerodynamic behaviour of small low Reynolds number axial turbine blades and provided a basis of better blade design.
219

The Measurement of Heat Flux from Igniters in Solid Propellant Rocket Motors

Siddiqui, K. M. January 1975 (has links)
No description available.
220

Heat exchanger network retrofit through heat transfer enhancement

Wang, Yufei January 2012 (has links)
Heat exchanger network retrofit plays an important role in energy saving in process industry. Many design methods for the retrofit of heat exchanger networks have been proposed during the last three decades. Conventional retrofit methods rely heavily on topology modifications which often results in a long retrofit duration and high initial costs. Moreover, the addition of extra surface area to the heat exchanger can prove difficult due to topology, safety and downtime constraints. These problems can be avoided through the use of heat transfer enhancement in heat exchanger network retrofit. This thesis develops a heuristic methodology and an optimization methodology to consider heat transfer enhancement in heat exchanger network retrofit. The heuristic methodology is to identify the most appropriate heat exchangers requiring heat transfer enhancements in the heat exchanger network. From analysis in the heuristic roles, some great physical insights are presented. The optimisation method is based on simulated annealing. It has been developed to find the appropriate heat exchangers to be enhanced and to calculate the level of enhancement required. The new methodology allows several possible retrofit strategies using different retrofit methods be determined. Comparison of these retrofit strategies demonstrates that retrofit modification duration and pay-back time are reduced significantly when only heat transfer enhancement is utilised. Heat transfer enhancement may increase pressure drop in a heat exchanger. The fouling performance in a heat exchanger will also be affected when heat transfer enhancement is used. Therefore, the implications of pressure drop and fouling are assessed in the proposed methodology predicated on heat transfer enhancement. Methods to reduce pressure drop and mitigate fouling are developed to promote the application of heat transfer enhancement in heat exchanger network retrofit. In optimization methodology considering fouling, the dynamic nature of fouling is simulated by using temperature intervals. It can predict fouling performance when heat transfer enhancement is considered in the network. Some models for both heat exchanger and heat transfer enhancement are used to predict the pressure drop performance in heat exchanger network retrofit. Reducing pressure by modifying heat exchanger structure is proposed in this thesis. From case study, the pressure drop increased by heat transfer enhancement can be eliminated by modifying heat exchanger structure.

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