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Two- and three-dimensional turbine blade row flow field simulationsWork performed in the numerical simulation of turbine passage flows via a Navier-Stokes approach is discussed. Both laminar and turbulent simulations in both two and three dimensions are discussed. An outline of the approach, background, and an overview of the results are given.
Document ID
19890007942
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Buggeln, R. C. (Scientific Research Associates, Inc. Glastonbury, CT, United States)
Briley, W. R. (Scientific Research Associates, Inc. Glastonbury, CT, United States)
Mcdonald, H. (Scientific Research Associates, Inc. Glastonbury, CT, United States)
Shamroth, S. J. (Scientific Research Associates, Inc. Glastonbury, CT, United States)
Weinberg, B. C. (Scientific Research Associates, Inc. Glastonbury, CT, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
89N17313
Funding Number(s)
CONTRACT_GRANT: NAS3-24358
CONTRACT_GRANT: NAS3-23695
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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