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Three-Dimensional Flow Analysis Inside Consortium Impeller at Design and Off-Design ConditionsThree-dimensional flow fields inside the Consortium impeller were analyzed with a Navier-Stokes code. The numerical results at the design and off-design conditions are compared with the experimental data.
Document ID
19950017203
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Hah, C. (NASA Lewis Research Center Cleveland, OH, United States)
Loellbach, J. (NASA Lewis Research Center Cleveland, OH, United States)
Tsung, F.-L. (NASA Lewis Research Center Cleveland, OH, United States)
Greenwald, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Garcia, Roberto (NASA Marshall Space Flight Center Huntsville, AL., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Publication Information
Publication: NASA. Marshall Space Flight Center, Eleventh Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
95N23623
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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