Optimal curved fibre orientations of a composite panel with cutout for improved buckling load using the Efficient Global Optimization algorithm
Author:
Affiliation:
1. Mechanical Engineering Department, Federal University of Technology – Paraná, Curitiba, Brazil
2. Institute for Aerospace Studies, University of Toronto, Toronto, Canada
Funder
Conselho Nacional de Desenvolvimento Científico e Tecnológico
Publisher
Informa UK Limited
Subject
Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications
Link
https://www.tandfonline.com/doi/pdf/10.1080/0305215X.2016.1256052
Reference40 articles.
1. ANSYS®. 2015a. ANSYS Composite PrepPost User's Guide. Canonsburg, PA: ANSYS.
2. ANSYS®. 2015b. ANSYS Mechanical User's Guide. Canonsburg, PA: ANSYS.
3. A formulation of general shell elements—the use of mixed interpolation of tensorial components
4. Design of variable-stiffness conical shells for maximum fundamental eigenfrequency
5. Optimization of a composite cylinder under bending by tailoring stiffness properties in circumferential direction
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