A new approach for evaluating fatigue lives of multi-fastener mechanical joints based on a nominal stress concept and minimal datasets

Author:

Tian B.J.,Xiong J.J.,Liu J.Z.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference26 articles.

1. Riveted lap joints in aircraft fuselage: design, analysis and properties;Andrzej,2012

2. Standard aircraft handbook for mechanics and technicians;Reithmaier,2014

3. Fatigue performance of production quality aircraft fastener holes;Ralph;Int J Fatigue,2007

4. Extending the fatigue life of multi-layer metal joints;Finney;Fatigue Fract Eng Mater Struct,1995

5. Cold expansion of holes and resulting fatigue life enhancement and residual stresses in Al 2024 T3 alloy – an experimental study;Gopalakrishna;Eng Fail Anal,2010

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