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Turbine stator flow field simulationsThe increased capability and accessibility of modern computers, coupled with increasingly sophisticated and accurate numerical and physical modeling, has led to a marked impact of numerical simulations upon current turbine design and research problems. The turbine section represents a considerable challenge as it contains significant regions of complex three-dimensional flow, including both aerodynamic and heat transfer phenomena. The focus of the present effort is the development of an efficient and accurate three-dimensional Navier-Stokes calculation procedure for application to the turbine stator and rotor problems. In particular, an effective procedure is sought which: (1) adequately represents the flow physics, (2) allows for sufficient resolution in regions of small length scale, and (3) has sufficiently good convergence properties so as to allow use on a regular basis.
Document ID
19890003531
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Buggeln, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Briley, W. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Shamroth, S. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcdonald, H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1986
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology 1986
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
89N12902
Funding Number(s)
CONTRACT_GRANT: NAS3-24358
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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