Unified Low Cycle Fatigue Model for Gas Turbine Engine Rotor Alloys
51st, AIAA/ASME/ASME/ASCE/AHS/ASC Structures, Stuctural Dynamics and Materials Conference ; 2010 ; Orlando, FL
2010-01-01
10 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Assessment of Current Turbine Engine High Cycle Fatigue Test Methods
Online Contents | 2003
|Turbine-Engine Transient-Rotor Analysis
NTRS | 1985
|Probabilistic High Cycle Fatigue Life Prediction for Gas Turbine Engine Blades
British Library Conference Proceedings | 1999
|