Evaluation of mixed mode-I/II criteria for fatigue crack propagation using experiments and modeling-Reference-Cited by-同舟云学术

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Evaluation of mixed mode-I/II criteria for fatigue crack propagation using experiments and modeling

Published:2018-07 Issue:7 Volume:31 Page:1525-1534
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

DEMIR Oğuzhan,AYHAN Ali O.,IRIC Sedat,LEKESIZ Hüseyin

Funder

Scientific and Technological Research Council of Turkey

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference38 articles.

1. High cycle fatigue in aircraft gas turbines-an industry perspective;Cowles;Int J Fract,1996

2. An assessment of the role of near-threshold crack growth in high-cycle-fatigue life prediction of aerospace titanium alloys under turbine engine spectra;Larsen;Int J Fract,1996

3. On the use of the Goodman diagram for high cycle fatigue design;Nicholas;Int J Fract,1996

4. Creep-fatigue failure of an aero engine turbine blades;Salam;Eng Fail Anal,2002

5. Innovative laser heating methodology study for crack growth retardation in aircraft structures;Yee;Int J Fatigue,2005

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4. Mixed-mode I&II fatigue crack growth behaviors of 16MND5 steel: The role of crack driving forces and crack closure;International Journal of Fatigue;2024-06

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