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A critical evaluation of a three-dimensional Navier-Stokes CFD as a tool to design supersonic turbine stagesThree-dimensional flow phenomena in a supersonic turbine blade row were studied numerically to evaluate CFD as a tool to design supersonic turbine stages. The details of the three-dimensional flow structure inside the supersonic turbine blade row and the overall aerodynamic performance at design and off-design conditions are analyzed and the results are compared between the experimental data and the numerical results.
Document ID
19920023024
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hah, C. (NASA Lewis Research Center Cleveland, OH, United States)
Kwon, O. (NASA Lewis Research Center Cleveland, OH, United States)
Shoemaker, M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 2
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N32268
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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