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A coupled multi-block solution procedure for spray combustion in complex geometriesTurbulent spray-combusting flow in complex geometries is presently treated by a coupled implicit procedure that employs finite-rate chemistry and real gas properties for combustion, as well as the stochastic separated model for spray and a multiblock treatment for complex geometries. Illustrative numerical tests conducted encompass a steady-state nonreacting backward-facing step flow, a premixed single-phase combustion flow, and spray combustion flow in a gas turbine combustor.
Document ID
19930040233
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chen, Kuo-Huey
(Toledo Univ.; NASA, Lewis Research Center Cleveland, OH, United States)
Shuen, Jian-Shun
(Sverdrup Technology, Inc.; NASA, Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-0108
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A24230
Distribution Limits
Public
Copyright
Other

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