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Optimized design of axial turbine rotor blades considering a wide range of attack angles

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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 extend the available range of attack angles and reduce profile loss, this paper develops a systematic aerodynamic optimization methodology for turbine blade profiles. This methodology integrates Latin Hypercube Sampling (LHS), Artificial Neural ...