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Turbine Aerodynamic Design System ImprovementsPresentation outline includes the following: 1. Volute manifold design and analysis methodology. 2. Meanline modification for compatibility with engine analysis code. Objective is to develop a manifold design methodology for turbines and pumps, and to enable rapid screening of candidate flow paths.
Document ID
20030062762
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Frank W Huber (Riverbend Design Services United States)
Lisa W Griffin (Marshall Space Flight Center Redstone Arsenal, United States)
Steven P Simpson (Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 21, 2013
Publication Date
April 1, 2003
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: Marshal Space Flight Center Fluids Workshop
Location: Birmingham, AL
Country: US
Start Date: April 22, 2003
End Date: April 24, 2003
Sponsors: Marshall Space Flight Center
Funding Number(s)
CONTRACT_GRANT: NASA Order H-35543-D
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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