Combined Cycle Fatigue of Gas Turbine Blade Materials at Elevated Temperature
Author:
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1475-1305.2009.00666.x/fullpdf
Reference7 articles.
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2. The contribution of advanced high-temperature materials to future aero-engines;Winstone;Proc. Inst. Mech. Eng, Part L, J Mat.,2001
3. Prediction of the combined high- and low-cycle fatigue performance of gas turbine blades after foreign object damage;Oakley;Int. J. Fat.,2007
4. Integrated approach for the development of advanced, coated gas turbine blades;Herzog;Adv. Eng. Mat.,2006
5. The Superalloys
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3. Threshold damage-based fatigue life prediction of turbine blades under combined high and low cycle fatigue;International Journal of Fatigue;2021-09
4. Dynamic fatigue reliability analysis of turbine blades under combined high and low cycle loadings;International Journal of Damage Mechanics;2021-01-17
5. Investigation on Material's Fatigue Property Variation Among Different Regions of Directional Solidification Turbine Blades—Part I: Fatigue Tests on Full Scale Blades;Journal of Engineering for Gas Turbines and Power;2014-07-22
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