Abstract The fatigue crack initiation and fatigue crack growth life estimations have been numerically investigated and the total estimated fatigue lives have been compared with available experimental fatigue test results for a single plate of aluminum 7075-T6 bolted with different applied torques. To do so, pre-stresses around the hole due to the torque tightened bolt and stress concentration factor of the combined longitudinally applied load and bolt clamping force were determined using 3D finite element simulations results. The calculated pre-stresses and stress concentration factors for different bolt clamping forces were employed in AFGROW computer package to predict fatigue crack initiation and fatigue crack growth lives. The results show that there is good agreement between the numerically predicted total fatigue lives and available experimental fatigue test results. The numerical results also show that bolt clamping force increases both fatigue crack initiation and fatigue crack growth lives individually.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Investigation of the fatigue life and crack growth in torque tightened bolted joints


    Contributors:

    Published in:

    Publication date :

    2010-08-05


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Spectrum fatigue of composite bolted joints

    Schon, J. / Nyman, T. | Tema Archive | 2002


    Pre-tensioning effect on fatigue life of bolted shear joints

    Benhaddou, Taha / Chirol, Clement / Daidie, Alain et al. | Elsevier | 2014



    Design Guidelines for Torque Controlled Tightening of Bolted Joints

    Eccles, William | SAE Technical Papers | 1993


    Design guidelines for torque controlled tightening of bolted joints

    Eccles,W. / WESTCOM,GB | Automotive engineering | 1993