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Effects of unsteady pulsating flows on the matching of a radial turbine with a spark-ignition engine

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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.
The matching of a radial inflow turbine with a piston engine, while ensuring torque backup across ranges of engine speeds and loads, is a complex task due to the nature of exhaust gas flows. This paper investigates the effects of pulsating exhaust gas ...