Riveted single lap joints Part 2: Fatigue life prediction

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 211, Issue 2, 1997, Pages 123-128

  Fung, C P ^a,b   Smart, J ^a  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

^b NATIONAL DEFENSE UNIVERSITY   (Taiwan)

Author keywords

Fatigue; Finite elements; Fretting; Lap joints; Riveted joints

Indexed keywords

FATIGUE OF MATERIALS; FATIGUE TESTING; FINITE ELEMENT METHOD; FRETTING CORROSION; MATHEMATICAL MODELS; PLASTICITY; RIVETS; STRAIN; STRESS ANALYSIS; STRUCTURAL LOADS;

RIVETED LAP JOINTS; STRESS LIFE LAW;

JOINTS (STRUCTURAL COMPONENTS);

FATIGUE LIFE ANALYSIS; FINITE ELEMENT ANALYSIS; FRETTING; JOINTS;

EID: 0030839121     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954410971532550     Document Type: Article

References (6)

1. Fung, C-P. and Smart, J. Riveted single lap joints. Part 1: a numerical parametric study. Proc. Instn Mech. Engrs, Part G, 1997, 211, 13-27.
2. Sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu4.4, Mg0.5, Si0.7, Mn0.8). British Standard BS 3L70, 1971 (British Standards Institution, London).
3. Fung, C-P. and Smart, J. An experimental and numerical analysis of riveted single lap joints. Proc. Instn Mech. Engrs, Part G, 1994, 208, 79-90.
4. Heywood, R. B. Designing against Fatigue, 1962, pp. 230-242 (Chapman and Hall Limited, London).
5. Heywood, R. B. Designing against Fatigue, 1962, pp. 159-160 (Chapman and Hall Limited, London).
6. Walker, K. The effect of stress ratio during crack propagation and fatigue- for 2024-T3 and 7075-T6 aluminium. Effects of Environment and Complex Load History on Fatigue Life, ASTM STP 462, 1970, pp. 1-14 (American Society of Testing and Materials).