Analysis of the Mechanical Properties of TC4-6061 Composite Plate Based on Classical Laminate Theory

Qiang Wang; Li Lin Liang; Chao Nan Peng

doi:10.4028/www.scientific.net/AMM.724.12

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 724Analysis of the Mechanical Properties of TC4-6061...

Analysis of the Mechanical Properties of TC4-6061 Composite Plate Based on Classical Laminate Theory

Abstract:

The calculation formula for the mechanical properties of TC4-6061 composite plate was deduced based on classical laminate theory. The stiffness, the strength, the specific stiffness and the specific strength for the plates was calculated by using the formula. The results show that with increasing of the relative thickness of titanium alloy layer, the tensile stiffness, the bending stiffness, the tensile strength and the bending strength increase rapidly, the tensile stiffness and tensile strength change little, the bending stiffness and specific bending strength first increase and then decrease.

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Periodical:

Applied Mechanics and Materials (Volume 724)

Pages:

12-16

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.724.12

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Online since:

January 2015

Authors:

Qiang Wang*, Li Lin Liang, Chao Nan Peng

Keywords:

Classical Laminate Theory, Mechanical Property, Titanium-Aluminum Composite Plate

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