Experimental and numerical investigations into the effect of an interference fit on the fatigue life of double shear lap joints

2009 ◽  
Vol 16 (7) ◽  
pp. 2066-2080 ◽  
Author(s):  
T.N. Chakherlou ◽  
M. Mirzajanzadeh ◽  
J. Vogwell
2014 ◽  
Vol 939 ◽  
pp. 39-46 ◽  
Author(s):  
Hong Qian Xue ◽  
Qian Tao ◽  
Emin Bayraktar

The aim of this study is to examine the effect of the clearance and interference-fit on the fatigue life of composite lap joints in double shear, 3D finite element simulations have been performed to obtain stress (or strain) distributions around the hole due to interference fit using FEM package, Non-linear contact analyses are performed to examine the effects of the clearance and interference for titanium and composite lap joint. Fatigue tests were conducted for the titanium and composite lap joints with clearance fit and interference fit with 0.5, 1, and 1.5% nominal interference fit levels at different cyclic loads. The results shows that interference fit increases fatigue life compared to clearance fit specimens, the titanium and composite lap joint with 1% interference fit level has the better fatigue life.


2013 ◽  
Vol 27 (5) ◽  
pp. 1415-1425 ◽  
Author(s):  
Hadi Taghizadeh ◽  
Tajbakhsh Navid Chakherlou ◽  
Afshin Babaei Aghdam

2021 ◽  
pp. 002199832110033
Author(s):  
B Abazadeh ◽  
HR Maleki

In this paper, the effect of bolt torque tightening has been investigated on the fatigue behavior of GLARE in double shear lap configuration. To do so, experimental fatigue tests were conducted using GLARE3-5/4-0.4 specimens with applied torques of 0 (finger tightened), 2 and 4 Nm at different cyclic longitudinal load ranges to achieve the stress-life (S-N) curves. The results revealed that applying and increasing the clamping force enhances the fatigue life of the GLARE specimens. Furthermore, comparison of fatigue test results of GLARE and available monolithic aluminum alloy 2024-T3 plates indicated when the applied load range is low, the effect of clamping force is more noticeable in GLARE specimens due to longer fatigue crack growth life of GLARE. Also, the occurrence of fretting fatigue didn’t reduce the fatigue life of GLARE specimens considerably in contrary to aluminum sheets because of the laminated structure of GLARE. The obtained results can provide insights in designing bolted GLARE joints with superior fatigue in-service performance.


2012 ◽  
Vol 96 ◽  
pp. 340-354 ◽  
Author(s):  
T.N. Chakherlou ◽  
H. Taghizadeh ◽  
M. Mirzajanzadeh ◽  
A.B. Aghdam
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