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Articles

A solution procedure for determining laminate configurations from lamination parameters

Pages 209-224 | Published online: 02 Apr 2012

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Read on this site (1)

Hisao Fukunaga, Hideki Sekine & Masahiro Hiragishi. (1994) Simultaneous optimization of shape and laminate configurations of laminated panels under multiple loadings. Advanced Composite Materials 3:3, pages 223-237.
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Articles from other publishers (7)

Yasser M. Meddaikar, François-Xavier Irisarri & Mostafa M. Abdalla. (2016) Laminate optimization of blended composite structures using a modified Shepard’s method and stacking sequence tables. Structural and Multidisciplinary Optimization 55:2, pages 535-546.
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S. White & P.M. Weaver. (2012) Bend-free shells under uniform pressure with variable-angle tow derived anisotropy. Composite Structures 94:11, pages 3207-3214.
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Shahriar Setoodeh, Mostafa M. Abdalla & Zafer G?rdal. (2006) Design of variable?stiffness laminates using lamination parameters. Composites Part B: Engineering 37:4-5, pages 301-309.
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Stuart Lemanski & Paul Weaver. (2006) Optimisation of a 4-layer laminated cylindrical shell to meet given cross-sectional stiffness properties. Composite Structures 72:2, pages 163-176.
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S. L. Lemanski, P. M. Weaver & G. F. J. Hill. (2016) Design of composite helicopter rotor blades to meet given cross-sectional properties. The Aeronautical Journal 109:1100, pages 471-475.
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Shahriar Setoodeh, Mostafa Abdallah, Zafer Gurdal & Brian Tatting. (2005) Design of Variable-Stiffness Composite Laminates for Maximum In-Plane Stiffness Using Lamination Parameters. Design of Variable-Stiffness Composite Laminates for Maximum In-Plane Stiffness Using Lamination Parameters.
Stuart Lemanski, Paul Weaver & Graham Hill. (2002) Design of Composite Cylindrical Shells to Meet Given Cross Sectional Stiffness Properties. Design of Composite Cylindrical Shells to Meet Given Cross Sectional Stiffness Properties.

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