NASA NTRS · 20050182985
RTF Analysis-Propulsion/Flowliner
Abstract
The 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.
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Kiris, Centin. 2004-01-01. RTF Analysis-Propulsion/Flowliner. https://ntrs.nasa.gov/citations/20050182985
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