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A throughflow optimizing strategy for axial compressor transition duct in a marine gas turbine

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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Published online on

Abstract

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
To enhance the aerodynamic performance of transition duct between low pressure and high pressure axial compressor for a gas turbine, a through-flow optimization strategy considering practical operating conditions is proposed in this paper. The method ...