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International Journal of Turbomachinery, Propulsion and Power
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International Journal of Turbomachinery, Propulsion and Power, Volume 3, Issue 2

2018 June - 9 articles

Cover Story: Aero engine design is based on the development of isolated components with fixed interface parameters and little or no feedback from other components. However, to guarantee consistent information transfer between all components and to fully exploit the optimization potential, holistic design goals should be pursued within a coupled, multi-objective, cooperative optimization framework through proper parametrization and optimization strategies.View Paper here.
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Int. J. Turbomach. Propuls. Power - ISSN 2504-186X
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