Failure mechanism of riveted joint in fibre metal laminates

Journal of Materials Processing Technology

Volumn 103, Issue 1, 2000, Pages 36-43

  Ryan, Liam ^a   Monaghan, John ^a  

^a TRINITY COLLEGE DUBLIN   (Ireland)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; COMPUTER SIMULATION; DELAMINATION; ELASTICITY; FAILURE ANALYSIS; FINITE ELEMENT METHOD; JOINTS (STRUCTURAL COMPONENTS); LAMINATED COMPOSITES; MATHEMATICAL MODELS; RIVETING; STRESS ANALYSIS; STRESS CONCENTRATION;

FIBRE METAL LAMINATES; RIVETED JOINTS;

FIBER REINFORCED METALS;

EID: 0033734274     PISSN: 09240136     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0924-0136(00)00416-7     Document Type: Article

References (5)

1. Vogelesang L.B., Gunnink J.W. ARALL: a material challenge for the next generation of aircraft. J. Mater. Design. 7:1986;20-30.
2. W.J. Slagter, Static strength of riveted joints in fibre metal laminates, Ph.D. Thesis, Department of Aerospace Engineering, Delft University, Netherlands, 1994.
3. R.P.G. Müller, An experimental and analytical investigation on the fatigue behaviour of fuselage riveted joints, Ph.D. Thesis, Department of Aerospace Engineering, Delft University, Netherlands, 1995.
4. L. Ryan, J. Monaghan, An investigation of the factors affecting the reliability of aircraft jointed structures, in: IMC 14, Proceedings of the 14th Conference of the Irish Manufacturing Committee, 1997, pp. 247-256.
5. L. Ryan, J. Monaghan, Interfacial pressure and stress distribution in a mechanical fastened joint, in: IMC 13, Proceeding of the 13th Conference of the Irish Manufacturing Committee, Re-Engineering for World Class Manufacturing, 1996, pp. 415-424.