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Combustor-diffuser interaction programA collection of empirical and analytical design methodology on combustor-diffuser systems was completed. A fully elliptic code was selected for analyzing the combustor-diffuser interaction. Analytical model predictions were obtained for all flow conditions at which Phase 2 tests will be conducted. These results will be compared with laser doppler velocimeter data. Furthermore, a generalized nonorthogonal grid system is being developed to accurately simulate complex wall shapes.
Document ID
19880001770
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Srinivasan, R.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
White, C.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA. Lewis Research Center, Turbine Engine Hot Section Technology, 1985
Subject Category
Aircraft Propulsion And Power
Accession Number
88N11152
Funding Number(s)
CONTRACT_GRANT: F33615-84-C-2427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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