Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response

Descriptions of fiber orientation variation for flat rectangular composite laminates that possess variable stiffness properties are introduced. The simplest definition employs a unidirectional variation based on a linear function for the fiber orientation angle of the individual layers. Analyses of...

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Bibliographic Details
Published in:	Composites. Part A, Applied science and manufacturing Vol. 39; no. 5; pp. 911 - 922
Main Authors:	Gürdal, Z., Tatting, B.F., Wu, C.K.
Format:	Journal Article
Language:	English
Published:	Kidlington Elsevier Ltd 01-05-2008 Elsevier
Subjects:	B. Buckling B. Elasticity Buckling C. Laminate mechanics E. Tow Exact sciences and technology Fundamental areas of phenomenology (including applications) Laminate design Physics Solid mechanics Structural and continuum mechanics E. Tow B. Buckling B. Elasticity C. Laminate mechanics Laminate design Laminate Mechanical properties Theoretical study Composite material Rayleigh Ritz method Rectangular plate Fiber orientation Stiffness Buckling
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