NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Simulation of a Single-Element Lean-Direct Injection Combustor Using Arbitrary Polyhedral MeshThis paper summarizes procedures of generating the arbitrary polyhedral mesh as well as presents sample results from its application to the numerical solution of a single-element LDI combustor using a preliminary version of the new OpenNCC.
Document ID
20120004158
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
August 25, 2013
Publication Date
January 9, 2012
Subject Category
Numerical Analysis
Report/Patent Number
E-18162
Report Number: E-18162
Meeting Information
Meeting: 50th AIAA ASM Conference
Location: Nashville, TN
Country: United States
Start Date: January 9, 2012
End Date: January 12, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.03.16.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available