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Determination of Mechanical Properties of Single and Double-Layer Intraply Hybrid Composites Manufactured by Hand Lay-Up Method. [PDF]
Shams M, Cakir F.
europepmc +1 more source
Effect of mesh sizes on the mechanical properties of stainless-steel wire mesh/glass fiber reinforced hybrid composite laminates for aerospace applications. [PDF]
Sayyed J, Ramprasad A, Pai Y.
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Recycling of Fiber-Metal Laminates
Fiber metal laminates provide superior mechanical properties over conventional metal alloys. However, they show a very poor recyclability due to its composite nature. Unique recycling technique is developed to recycle both the glass fiber and the aluminum alloy. The process consists of a thermal delamination and an alloy refining step.
Yong Xiang Yang +2 more
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Optimal Strength Design for Fiber-Metal Laminates and Fiber-reinforced Plastic Laminates
Optimal strength design of fiber-reinforced plastic (FRP) laminates and fiber-metal laminates (FML) is studied in this article. An optimization approach that integrates the particle swarm optimization algorithm and a general finite element code ANSYS was developed.
null Wenjie Peng +3 more
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The Bearing Strength of Fiber Metal Laminates
Journal of Composite Materials, 2006The bearing strength, in particular the edge distance sensitivity, of several fiber metal laminates of the GLARE family is experimentally evaluated. The behavior of the fiber layer is investigated in detail to obtain a better understanding of its failure mode.
J Sinke, Sybrand Van Der Zwaag
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Forming and drilling of fiber metal laminates – A review
In aviation industries, most of the stiffened structural components are manufactured by forming and laminating process. Combination of several conventional manufacturing processes is required in modern industries in hybrid laminate production. Fiber metal laminates undergo various joining process during assembly of aero-structures.
M Thirukumaran +3 more
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Investigation on Formability of Fiber Metal Laminates [PDF]
In this study, the formability of fiber metal laminates (FML) used in aerospace industry were experimentally examined. Al5754-H22 sheets in two different thicknesses (0.6 and 1.2 mm) were used in top and bottom layers of FML specimens. Carbon fiber plates made of prepreg carbon fiber fabrics were placed in the middle layer of FML specimens. In order to
IŞIKTAŞ, Ali, TAŞKIN, Vedat
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