Static Strength Comparison of Riveted versus Friction Stir Welded Stiffened Panels

Author(s):  
Bryan Tweedy ◽  
Scott Sellmeyer ◽  
Adam Jahn ◽  
Dwight Burford
2005 ◽  
Author(s):  
Anil K. Patnaik ◽  
Josh Schurger ◽  
Annicia Streete ◽  
Casey D. Allen ◽  
William J. Arbegast

Author(s):  
Amirreza Shahani ◽  
Ali Farrahi

The effect of five different stirring times of friction stir spot welding on lap-shear specimens of Al 6061-T6 alloy has been experimentally analyzed. The welding condition with 2 s of stirring shows the optimum mechanical behavior in comparison to the others. The static strength and fatigue behavior of the joint are justified using the microhardness profiles. The static results prove that the increase of stirring time beyond the 2 s case has little effect on improving the static strength. The fatigue results reveal two different failure modes, which are shear fracture at high load levels and transverse crack growth at low load levels. At medium load levels, although the final failure is similar to high load levels, the transverse growth of the crack outside the welding zone, just like low load levels, is also observed.


Author(s):  
A Murphy ◽  
T Ekmekyapar ◽  
M Özakça ◽  
K Poston ◽  
G Moore ◽  
...  

Materials ◽  
2019 ◽  
Vol 12 (11) ◽  
pp. 1785 ◽  
Author(s):  
Andrzej Kubit ◽  
Tomasz Trzepiecinski ◽  
Łukasz Święch ◽  
Koen Faes ◽  
Jan Slota

Many aircraft structures are thin walled and stringer-stiffened, and therefore, prone to a loss of stability. This paper deals with accurate and validated stability analysis of the model of aircraft skin under compressive loading. Both experimental and numerical analyzes are conducted. Two different methods of joining panel elements are considered. In the first case, the panel is fabricated using rivets. In the second variant, the refill friction stir spot welding technique is used. Both types of panels are loaded in axial compression in a uniaxial tensile testing machine. The geometrically and physically nonlinear finite element analyzes of the panels were carried out in ABAQUS/Standard. The Digital Image Correlation measurement system ARAMIS has been utilized to monitor the buckling behavior and failure mode in the skin-stringer interface of the stiffened panels. The results of experiments and the digital image correlation system are presented and compared to the numerical simulations.


2008 ◽  
Vol 5 (4) ◽  
pp. 101568 ◽  
Author(s):  
Dwight A. Burford ◽  
Bryan M. Tweedy ◽  
Christian A. Widener ◽  
R. W. Neu ◽  
K. R. W. Wallin ◽  
...  

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