This 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).
Updates to Simulation of a Single-Element Lean-Direct Injection Combustor Using Arbitary Polyhedral Meshes
AIAA SciTech 2015 ; 2015 ; Kissimmee, FL, United States
2015-01-05
Conference paper
No indication
English
Aerodynamics , Propulsion , Aircraft , Power
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2014
|Simulation of a Single-Element Lean-direct Injector Combustor Using Arbitrary Polyhedral Mesh
British Library Conference Proceedings | 2012
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