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The impact of separated flow on heat and mass transfer. Final report

Description: An investigation of the effect of flow separation on heat and mass transfer has been completed. This research provided enhanced understanding of fundamental mechanisms governing important heat and mass transfer flow processes. This report summarizes the work conducted under the project. This research has provided considerable new knowledge on flow and heat transfer situations of great interest in a number of energy conversion devices, including heat exchangers, gas turbines, solar energy systems and general heat transfer systems.
Date: August 1, 1998
Creator: Goldstein, R.J.
Partner: UNT Libraries Government Documents Department

The impact of separated flow on heat and mass transfer

Description: An investigation of the effect of flow separation on heat (or mass) transfer is underway. This research, sponsored by the Department of Energy (Contract No. FG02-87ER13800), is planned to enhance our understanding of the fundamental mechanisms governing the process. This report summarizes previous accomplishments and briefly describes works done during period May 1, 1989 through April 30, 1990. Future plans and studies under preparation are also mentioned. 8 refs., 7 figs.
Date: January 1, 1990
Creator: Goldstein, R.J. & Jabbari, M.Y.
Partner: UNT Libraries Government Documents Department

Experimental and computational studies of film cooling with compound angle injection

Description: The thermal efficiency of gas turbine systems depends largely on the turbine inlet temperature. Recent decades have seen a steady rise in the inlet temperature and a resulting reduction in fuel consumption. At the same time, it has been necessary to employ intensive cooling of the hot components. Among various cooling methods, film cooling has become a standard method for cooling of the turbine airfoils and combustion chamber walls. The University of Minnesota program is a combined experimental and computational study of various film-cooling configurations. Whereas a large number of parameters influence film cooling processes, this research focuses on compound angle injection through a single row and through two rows of holes. Later work will investigate the values of contoured hole designs. An appreciation of the advantages of compound angle injection has risen recently with the demand for more effective cooling and with improved understanding of the flow; this project should continue to further this understanding. Approaches being applied include: (1) a new measurement system that extends the mass/heat transfer analogy to obtain both local film cooling and local mass (heat) transfer results in a single system, (2) direct measurement of three-dimensional turbulent transport in a highly-disturbed flow, (3) the use of compound angle and shaped holes to optimize film cooling performance, and (4) an exploration of anisotropy corrections to turbulence modeling of film cooling jets.
Date: December 31, 1995
Creator: Goldstein, R.J.; Eckert, E.R.G.; Patankar, S.V. & Simon, T.W.
Partner: UNT Libraries Government Documents Department