Numerical Study of the Effective Lap-Splice Length of FRCM Composites

2021 ◽  
pp. 213-223
Author(s):  
Tommaso D’Antino ◽  
Angelo Savio Calabrese ◽  
Pierluigi Colombi ◽  
Carlo Poggi
Keyword(s):  
Author(s):  
Paul M. Gioioso ◽  
Jorge Rodriguez

Abstract A study was performed to assess the effect of multiple site damage (MSD), which has been observed in a number of aging aircraft, on the fatigue life of lap splice joints in fuselage structures. Numerical modeling was used to simulate various MSD occurrences in models similar to riveted aircraft structures (e.g. rows of 5/32″ diameter holes separated by a finite distance, for a T2024-T3 aluminum material) under simulated fatigue loading. Several geometric factors were examined, and their effect on MSD propagation investigated. Nonuniform MSD was also modeled, and all effects were compared on a global scale. Results indicate that a tighter array configuration allowed for a shorter fatigue life, as did the introduction of the nonuniform crack. However, the effect of the staggered offset was negligible in comparison to the effect of the rivet spacing and the location of the nonuniform crack. The size and initial location of the nonuniform crack had the greatest influence on the stress distribution and the fatigue life.


2013 ◽  
Vol 40 (11) ◽  
pp. 1140-1149 ◽  
Author(s):  
Ramin Rameshni ◽  
Stefano Arcovio ◽  
Mark Green ◽  
Colin MacDougall

This study investigates, experimentally and using finite element analysis, the adhesive bond between glass fibre-reinforced polymer (GFRP) and steel. Seventeen double-shear lap-splice were fabricated and tested in tension. The results show that the methacrylate adhesive used had higher bond strengths than the epoxy adhesive. A finite element model for selected test specimens was developed to analyze the stress within the adhesive. The model was verified by comparison with strain data from the shear lap-splice tests. The model was used to determine the maximum principal stress in the epoxy adhesive and the maximum shear strain in the methacrylate adhesive at failure, and thus quantify the characteristic strength of these adhesives. It was shown that the ductility of the methacrylate adhesive allowed it to yield at locations of stress concentrations, providing higher splice capacity, despite having a lower nominal shear strength as compared with the epoxy adhesive.


1998 ◽  
Vol 77 (2) ◽  
pp. 473-484 ◽  
Author(s):  
M. Sampoli, P. Benassi, R. Dell'Anna,

2020 ◽  
pp. 57-65
Author(s):  
Eusébio Conceiçã ◽  
João Gomes ◽  
Maria Manuela Lúcio ◽  
Jorge Raposo ◽  
Domingos Xavier Viegas ◽  
...  

This paper refers to a numerical study of the hypo-thermal behaviour of a pine tree in a forest fire environment. The pine tree thermal response numerical model is based on energy balance integral equations for the tree elements and mass balance integral equation for the water in the tree. The simulation performed considers the heat conduction through the tree elements, heat exchanges by convection between the external tree surfaces and the environment, heat exchanges by radiation between the flame and the external tree surfaces and water heat loss by evaporation from the tree to the environment. The virtual three-dimensional tree model has a height of 7.5 m and is constituted by 8863 cylindrical elements representative of its trunks, branches and leaves. The fire front has 10 m long and a 2 m high. The study was conducted taking into account that the pine tree is located 5, 10 or 15 m from the fire front. For these three analyzed distances, the numerical results obtained regarding to the distribution of the view factors, mean radiant temperature and surface temperatures of the pine tree are presented. As main conclusion, it can be stated that the values of the view factor, MRT and surface temperatures of the pine tree decrease with increasing distance from the pine tree in front of fire.


2013 ◽  
Author(s):  
Pancheewa Benjamasutin ◽  
◽  
Ponthong Rijana ◽  
Phongchayont Srisuwan ◽  
Aussadavut Dumrongsiri

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