NASA NTRS · 19930040233
A coupled multi-block solution procedure for spray combustion in complex geometries
Abstract
Turbulent 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.
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Chen, Kuo-Huey, Shuen, Jian-Shun. 1993-01-01. A coupled multi-block solution procedure for spray combustion in complex geometries. https://ntrs.nasa.gov/citations/19930040233
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