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- W1506726185 abstract "The creep fatigue behavior of a fully impingement cooled blade for four cyclic cases was analyzed by using the Elas 55, finite element, nonlinear structural computer program. Expected cyclic lives were calculated by using the method of strainrange partitioning for reversed inelastic strains and time fractions for ratcheted tensile creep strains. Strainrange partitioning was also applied to previous results from a one dimensional cyclic analysis of a film impingement cooled vane. The analyses indicated that strainrange partitioning is more applicable to a constrained airfoil such as the film impingement cooled vane than to the relatively unconstrained fully impingement cooled airfoil." @default.
- W1506726185 created "2016-06-24" @default.
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- W1506726185 date "1976-02-01" @default.
- W1506726185 modified "2023-09-26" @default.
- W1506726185 title "Cyclic Structural Analyses of Air-Cooled Gas Turbine Blades and Vanes" @default.
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- W1506726185 doi "https://doi.org/10.4271/760918" @default.
- W1506726185 hasPublicationYear "1976" @default.
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