The paper presents a novel experimental procedure and local approach model for assessing the thermo-mechanical fatigue behavior of the trailing edge root for gas turbine blades. The methodology can be successfully used for defining life assessment models including geometrical features and manufacturing process effects.

High temperature fatigue behavior of GT blades in the trailing edge root

macoretta g.
Writing – Original Draft Preparation
;
monelli b. d.
Primo
Writing – Review & Editing
;
bertini l.;santus c.;beghini m.;
2018-01-01

Abstract

The paper presents a novel experimental procedure and local approach model for assessing the thermo-mechanical fatigue behavior of the trailing edge root for gas turbine blades. The methodology can be successfully used for defining life assessment models including geometrical features and manufacturing process effects.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11568/1116856
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