Author:
Mishra R. K.,Kishore Kumar S.,Chandel Sunil
Abstract
AbstractLean blow out characteristics in a swirl stabilized aero gas turbine combustor have been studied using computational fluid dynamics. For CFD analysis, a 22.5° sector of an annular combustor is modeled using unstructured tetrahedral meshes comprising 1.2 × 10
Cited by
16 articles.
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