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RTF Analysis-Propulsion/FlowlinerThe objective of the current task is to provide a computational framework for design and analysis of the entire fuel supply system of a liquid rocket engine, including high fidelity unsteady turbopump flow analysis. Time-accurate results obtained from shuttle fuel flowliner analysis using 66 Million grid points with 262 overlapped zones will be shown. We will present analysis results along with performance data of the simulation runs on Supercomputers such as Columbia.
Document ID
20050182985
Acquisition Source
Headquarters
Document Type
Abstract
Authors
Kiris, Centin (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Supercomputing 2004
Location: Pittsburgh, PA
Country: United States
Start Date: November 6, 2004
End Date: November 12, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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