Effect of Diffuser Bleed on Performance of an Annular Swirl Can Combustor
Author : Albert J. Juhasz
Publisher :
Page : 28 pages
File Size : 22,63 MB
Release : 1974
Category : Aircraft gas-turbines
ISBN :
Author : Albert J. Juhasz
Publisher :
Page : 28 pages
File Size : 22,63 MB
Release : 1974
Category : Aircraft gas-turbines
ISBN :
Author : John Milton Smith
Publisher :
Page : 24 pages
File Size : 11,66 MB
Release : 1979
Category : Diffusers
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Author :
Publisher :
Page : 364 pages
File Size : 47,37 MB
Release : 1975
Category : Aeronautics
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Author : John Milton Smith
Publisher :
Page : 24 pages
File Size : 50,15 MB
Release : 1979
Category : Diffusers
ISBN :
Author :
Publisher :
Page : 1126 pages
File Size : 44,53 MB
Release : 1987
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : J.M. Smith
Publisher :
Page : pages
File Size : 12,56 MB
Release : 1979
Category :
ISBN :
Author : Albert J. Juhasz
Publisher :
Page : 28 pages
File Size : 29,32 MB
Release : 1971
Category : Combustion chambers
ISBN :
Velocity profile control tests were conducted with a short annular diffuser equipped with wall bleed capability. The diffuser area ratio was 4, and the length to inlet height ratio was 1. 5. Results show that the diffuser radial exit velocity profile may be shifted towards either the inner or outer diffuser wall by, respectively, bleeding off a small fraction of the total flow through the inner or outer wall. Based on these results, application of the diffuser bleed technique to a gas turbine combustor should be considered. The advantages of such a combustor could be shorter length, reduced idle exhaust emissions, and improved altitude relight capability.
Author :
Publisher :
Page : 952 pages
File Size : 46,17 MB
Release : 1975
Category : Mechanics, Applied
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Author : Albert J. Juhasz
Publisher :
Page : 38 pages
File Size : 12,36 MB
Release : 1975
Category : Aircraft gas-turbines
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Author : Oak Ridge National Laboratory
Publisher :
Page : 1356 pages
File Size : 32,39 MB
Release : 1976
Category : Power resources
ISBN :