A throughflow optimizing strategy for axial compressor transition duct in a marine gas turbine
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Published online on April 07, 2026
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 ...
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 ...