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An Inducer CFD Solution and Effects Associated with CavitationThis presentation describes a CFD analysis for an Alternate Turbopump Development (ATD) configuration. The analysis consists of a coupled configuration of the inducer and impeller. The work presented here is a joint collaboration of J. Garrett, J. Kuryla and myself.
Document ID
19950017211
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Pervaiz, Mehtab M. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Garrett, J. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Kuryla, J. (Pratt and Whitney Aircraft West Palm Beach, FL, 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
95N23631
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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