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Fatigue-creep design of transpiration cooled nickel gas turbine blades via low order aerothermal-stress and crystal plasticity finite element modelling (2025)

First Author: Skamniotis C

Attributed to: Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.ijmecsci.2025.109955

Publication URI: http://dx.doi.org/10.1016/j.ijmecsci.2025.109955

Type: Journal Article/Review

Parent Publication: International Journal of Mechanical Sciences

ISSN: 00207403