Optimized design of axial turbine rotor blades considering a wide range of attack angles
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Published online on March 21, 2026
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 ...
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 ...