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Prediction of turbine blade heat transferIt is planned to incorporate a number of low Reynolds number turbulence models in a general two-dimensional boundary layer calculation procedure. This will be applied to different flow conditions over turbine blades and the predictions will be compared with experimental data. The prediction activity will lead to a recommendation about a satisfactory turbulence model for turbine blade heat transfer.
Document ID
19880001780
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Patankar, Suhas V.
(Minnesota Univ. Minneapolis, MN, 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
Fluid Mechanics And Heat Transfer
Accession Number
88N11162
Funding Number(s)
CONTRACT_GRANT: NAG3-579
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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