Damage mechanics method for fatigue life prediction of Pitch-Change-Link

International Journal of Fatigue

Volumn 32, Issue 10, 2010, Pages 1683-1688

  Zhang, Miao ^a   Meng, Qingchun ^a   Hu, Weiping ^a   Shi, Sidian ^b   Hu, Maohe ^b   Zhang, Xing ^a  

^a BEIHANG UNIVERSITY   (China)

^b Chinese Helicopter Research and Development Institute   (China)

Author keywords

ANSYS; Damage mechanics; Fatigue life; Pitch Change Link

Indexed keywords

ANSYS PLATFORM; APDL LANGUAGE; CLOSED-FORM RELATIONS; DAMAGE EVOLUTION EQUATION; DAMAGE MECHANICS; EXPERIMENT DATA; EXPERIMENTAL DATA; FATIGUE CRACK INITIATION; FATIGUE LIFE; FATIGUE LIFE PREDICTION; MATERIAL PARAMETER; MAXIMUM STRESS; NEW DAMAGE; NOTCHED SPECIMENS; REPEATED LOADING; STANDARD SPECIMENS; STRAIN AMPLITUDE;

CRACK INITIATION; CRACKS; DIFFERENTIAL EQUATIONS; FINITE ELEMENT METHOD; FORECASTING; MECHANICS;

FATIGUE DAMAGE;

EID: 77955266917     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2010.04.001     Document Type: Article

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