Publication Date:
2019-08-13
Description:
The low emissions potential of a Rich-Quench-Lean (RQL) combustor for use in the HIgh Speed Civil transport (HSCT) application was evaluated as part of the NASA Critical Propulsion Components (CPC) Program. Fuel shifting as an approach to combustor control was evaluated in a multiple bank RQL combustor, utilizing reduced scale quench technology implemented in a convoluted linear with quench plate concept.
Keywords:
Aircraft Propulsion and Power
Type:
NASA/CR-2004-212879
,
E-14293
Format:
application/pdf
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