A unified prediction model for physically small crack and long crack growth based on modified CTOD

Author:

Zhang Wei,Chai Lindong,Ren Luping,Cai Liang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference53 articles.

1. Roles of microstructure in fatigue crack initiation;Chan;Int J Fatigue,2010

2. Defects as a root cause of fatigue failure of metallic components. I: basic aspects;Zerbst;Eng Failure Anal,2019

3. Short fatigue crack behaviour and analytical models: a review;Hussain;Eng Fract Mech,1997

4. Characterisation of equivalent initial flaw sizes in 7050 aluminium alloy;Molent;Fatigue Frac Eng Mater Struct,2006

5. Schijve J. Fatigue life until small cracks in aircraft structures: durability and damage tolerance. NASA Langley Research Center, FAA (NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerane, Part 21994.

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