Prediction of fatigue life in aircraft double lap bolted joints using several multiaxial fatigue criteria

Materials and Design

Volumn 59, Issue , 2014, Pages 430-438

  Esmaeili, F ^a   Chakherlou, T N ^a   Zehsaz, M ^a  

^a UNIVERSITY OF TABRIZ   (Iran)

Author keywords

Bolted joint; Clamping force; Finite element; Multiaxial fatigue; Torque tightening

Indexed keywords

BOLT TIGHTENING; BOLTED JOINTS; CLAMPING DEVICES; FATIGUE TESTING; FINITE ELEMENT METHOD; TORQUE;

2024-T3 ALUMINIUM; CLAMPING FORCE; FATIGUE STRENGTH; MULTI-AXIAL FATIGUE; MULTIAXIAL FATIGUE CRITERIA; NON-LINEAR FINITE ELEMENTS; PREDICTION OF FATIGUE LIVES; STRESS AND STRAIN DISTRIBUTION;

FATIGUE OF MATERIALS;

EID: 84897465315     PISSN: 02613069     EISSN: 18734197     Source Type: Journal    
DOI: 10.1016/j.matdes.2014.03.019     Document Type: Article

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