A combustor assembly includes a combustor vessel having a wall, a proximate end defining an opening and a closed distal end opposite said proximate end. A manifold is carried by the proximate end. The manifold defines a combustion products exit. The combustion products exit being axially aligned with a portion of the closed distal end. A plurality of combustible reactant ports is carried by the manifold for directing combustible reactants into the combustion vessel from the region of the proximate end towards the closed distal end.
Stagnation point reverse flow combustor for a combustion system
2007-01-30
Miscellaneous
No indication
English
LES of Premixed Combustion in the Stagnation Point Reverse Flow Combustor
British Library Conference Proceedings | 2006
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