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Procedure for Determining One-Dimensional Flow Distributions in Arbitrarily Connected Passages Without the Influence of PumpingA calculation procedure is presented which allows the one-dimensional determination of flow distributions in arbitrarily connected (branching) flow passages having multiple inlets and exits. The procedure uses an adaptation of the finite element technique, iteratively coupled with an accurate one-dimensional flow solver. The procedure eliminates the usual restrictions inherent with finite element flow calculations. Unlike existing one-dimensional methods, which require simplifications to the flow equations (uncoupling the momentum and energy equations), to allow for arbitrary branching and multiple inlets and exits, the only limitation of the described methodology is that, at present, it can only accommodate non-rotating configurations (no pumping effects). The calculation procedure is robust, and will always converge for physically possible flow. The procedure is described, and its use is illustrated by an example.
Document ID
20040082327
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Meitner, Peter L.
(Army Research Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2004-211885
E-13567
GT2003-38061
ARL-TR-3213
Report Number: NASA/TM-2004-211885
Report Number: E-13567
Report Number: GT2003-38061
Report Number: ARL-TR-3213
Meeting Information
Meeting: Turbo Expo 2003
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2003
End Date: June 19, 2003
Sponsors: International Gas Turbine Inst., American Society of Mechanical Engineers
Funding Number(s)
PROJECT: DA Proj. 1L1-61102-AF-20
WBS: WBS 22-722-90-C1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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