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An investigation of the effect of inlet-swirl on the flow through a micro-gas turbine combustion chamber
(Stellenbosch : Stellenbosch University, 2016-03)
ENGLISH ABSTRACT: Previous research on the BMT120-KS micro-gas turbine engine has revealed that there is a component of swirl present at the compressor outlet. The effect of this inlet swirl on the flow through a micro-gas ...