Numerical simulation of noise attenuating perforated combustor liners and the combustion instability issue in gas turbine engines
Combustion instability represents a significant problem in the application of low emission lean premixed combustion for gas turbines and has become one of the primary concerns in modern gas turbine industry. Effusion cooling has become common practice in gas turbine combustors and when calibrated, p...
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University of Hull
2017
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| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.733013 |