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Simulation of a Single-Element Lean-Direct Injection Combustor Using a Polyhedral Mesh Derived from Hanging-Node ElementsThis paper summarizes the procedures of generating a polyhedral mesh derived from hanging-node elements as well as presents sample results from its application to the numerical solution of a single element lean direct injection (LDI) combustor using an open-source version of the National Combustion Code (NCC).
Document ID
20150009940
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Wey, Thomas (NASA Glenn Research Center Cleveland, OH, United States)
Liu, Nan-Suey (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 5, 2015
Publication Date
January 7, 2013
Subject Category
Numerical Analysis
Aircraft Propulsion And Power
Report/Patent Number
E-664427
Report Number: E-664427
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: Grapevine, TX
Country: United States
Start Date: January 7, 2013
End Date: January 10, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 794072.02.03.05.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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