Title of article
Mechanical Properties of RTM-made Composite Cross-joints
Author/Authors
Cheng، نويسنده , , Xu and Xiong، نويسنده , , Junjiang and Peng، نويسنده , , Bo and Cheng، نويسنده , , Zeling and Li، نويسنده , , Hongyun، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2009
Pages
7
From page
211
To page
217
Abstract
Tension and shear tests are carried out on composite cross-joints, produced by resin transfer moulding (RTM), stitch-RTM and cobonding techniques separately, to investigate the influences of different production methods on their mechanical properties and their failure mechanism. It is concluded from test results that, in terms of mechanical properties, the RTM-made cross-joint holds superiority over other two, and both stitch-RTM and cobonding methods have significant adverse effects on mechanical properties. Experimental observation and finite element (FE) numerical simulation show that the delamination first takes place at the upper triangle-like resin-rich zone of joints, then propagates along the interface between the zone and the curved webs/flanges to the bottom plate, and grows along the horizontal bottom plate till failure of the joint accurs at last. Results demonstrate that there is a good agreement between the FE model and the tests.
Keywords
Composites , resin transfer moulding (RTM) , mechanical properties , cross-joint , stitching , Numerical simulation , cobonding
Journal title
Chinese Journal of Aeronautics
Serial Year
2009
Journal title
Chinese Journal of Aeronautics
Record number
2264794
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