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Updates to Simulation of a Single-Element Lean-Direct Injection Combustor Using Arbitary Polyhedral MeshesThis paper summarizes the procedures of (1) generating control volumes anchored at the nodes of a mesh; and (2) generating staggered control volumes via mesh reconstructions, in terms of either mesh realignment or mesh refinement, as well as presents sample results from their applications to the numerical solution of a single-element LDI combustor using a releasable edition of the National Combustion Code (NCC).
Document ID
20150002854
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
March 13, 2015
Publication Date
January 5, 2015
Subject Category
Aerodynamics
Report/Patent Number
GRC-E-DAA-TN19583
Report Number: GRC-E-DAA-TN19583
Meeting Information
Meeting: AIAA SciTech 2015
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
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.
Keywords
Power
Aircraft
Propulsion
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