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Updates to Simulation of a Single-Element Lean-Direct Injection Combustor Using a Polyhedral Mesh Derived From Hanging-Node ElementsThis paper summarizes the procedures of inserting a thin-layer mesh to existing inviscid polyhedral mesh either with or without hanging-node elements as well as presents sample results from its applications to the numerical solution of a single-element LDI combustor using a releasable edition of the National Combustion Code (NCC).
Document ID
20140012698
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Wey, Changju Thomas (NASA Glenn Research Center Cleveland, OH, United States)
Liu, Nan-Suey (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 29, 2014
Publication Date
March 1, 2014
Subject Category
Aerodynamics
Aircraft Propulsion And Power
Report/Patent Number
E-18839
NASA/TM-2014-218108
Meeting Information
Meeting: Science and Technology Forum and Exposition (SciTech2014)
Location: National Harbor, MD
Country: United States
Start Date: January 13, 2014
End Date: January 17, 2014
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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