Fundamental Study of Three Dimensional Two-phase Flow in Combustion Systems
Author : Ewan and Swithenbank
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Page : pages
File Size : 47,75 MB
Release : 1987
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Author : Ewan and Swithenbank
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Page : pages
File Size : 47,75 MB
Release : 1987
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Page : 702 pages
File Size : 36,1 MB
Release : 1995
Category : Aeronautics
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Page : 354 pages
File Size : 33,47 MB
Release : 1993
Category : Power resources
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Page : 900 pages
File Size : 20,20 MB
Release : 1985
Category : Power resources
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Semiannual, with semiannual and annual indexes. References to all scientific and technical literature coming from DOE, its laboratories, energy centers, and contractors. Includes all works deriving from DOE, other related government-sponsored information, and foreign nonnuclear information. Arranged under 39 categories, e.g., Biomedical sciences, basic studies; Biomedical sciences, applied studies; Health and safety; and Fusion energy. Entry gives bibliographical information and abstract. Corporate, author, subject, report number indexes.
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Page : 188 pages
File Size : 13,79 MB
Release : 1982
Category : Science
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Page : 676 pages
File Size : 45,2 MB
Release : 1985
Category : Power resources
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Page : 1242 pages
File Size : 39,53 MB
Release : 1985
Category : Government reports announcements & index
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Page : 1036 pages
File Size : 30,39 MB
Release : 1985-05
Category : Science
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Page : 1072 pages
File Size : 31,26 MB
Release : 1986
Category : Mechanics, Applied
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Author : B. Ewan
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Page : 6 pages
File Size : 26,50 MB
Release : 1981
Category : Internal combustion engines
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A fundamental approach to combustor modelling is being extended by the coupling of combustor flow fields and fuel droplet trajectories. The iterative procedures, which have been applied to a gas turbine, evaluate reacting flow fields and indicate the conditions under which fuel is able to escape incompletely evaporated from the burner. Important advances have also been made in the application of a valid turbulence model to the calculation of flow fields in non-isotropic swirling flows. This has important implications for combustor designing for a wide range of systems including gas turbines and ramjets. The development of a non-intrusive and rapid method for residence time distribution measurement has progressed to the point of application to a gas turbine combustor. This involves the optical detection of an electrically generated pulse of mercury vapour and can give residence times in real time. (Author).