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

Author:

Chakherlou T.N.,Mirzajanzadeh M.,Vogwell J.,Abazadeh B.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. A. Atre, A finite element and experimental investigation on the fatigue of riveted lap joints in aircraft applications, PhD thesis, Georgia Institute of Technology, 2006, pp. 97–100.

2. Effect of corrosion severity on fatigue evolution in Al–Zn–Mg–Cu;Burns;Corrosion Science,2010

3. T.N. Chakherlou, An evaluation of cold expansion methods used for improving the fatigue life of fastener holes in aerospace aluminium alloy 7075-T6, PhD thesis, University of Bath, 2002, pp. 88–111.

4. The effect of bolt clamping force on the fracture strength and the stress intensity factor of a plate containing a fastener hole with edge cracks;Chakherlou;Eng. Fail. Anal.,2009

5. An investigation about interference fit effect on improving fatigue life of a holed single plate in joints;Chakherlou;Eur. J. Mech. A Solids,2010

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