Design of variable–stiffness laminates using lamination parameters
By Shahriar Setoodeh, Mostafa Abdalla, Zafer Gürdal. 2006
271 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/808e29486528cfd7935e25beb18ec226da8c3a49
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Civil and Structural Engineering
- Kazem Fayazbakhsh
- Damiano Pasini
- L. Lessard
- M. A. Nik
- Zafer Gürdal
- Hossein Ghiasi
- Mostafa Abdalla
- Samuel T. IJsselmuiden
In Mechanics of Materials
- Kazem Fayazbakhsh
- Damiano Pasini
- L. Lessard
- M. A. Nik
- Hossein Ghiasi
- Mostafa Abdalla
- Samuel T. IJsselmuiden
- Zafer Gürdal
Citations in the corpus
- Optimum stacking sequence design of composite materials Part I: Constant stiffness design (2009, background): “[6], in which there are two scenarios for the design of a composite structure:”
- Optimization of Variable-Stiffness Panels for Maximum Buckling Load Using Lamination Parameters (2010, background): “In past research the generalized reciprocal approximation, in which the response is approximated based on the inverse of the stiffness tensors, has been successful for variable-stiffness design [9,26].”
- Surrogate-based multi-objective optimization of a composite laminate with curvilinear fibers (2012, unknown): “All rights reserved.”
- Optimum stacking sequence design of composite materials Part II: Variable stiffness design (2010, methodology): “[89] used this formulation and considered the minimum compliance energy as optimality criteria.”
- Material extrusion additive manufacturing of continuous fibre reinforced polymer matrix composites: A review and outlook (2021, background): “These areas of research were focused on improving buckling properties of cylindrical structures such as fuselages and stiffened panel with cut-outs by making use of fibre steering [49, 50, 168, 64, 65, 143, 141, 142, 92].”
- Optimization of variable stiffness composites with embedded defects induced by Automated Fiber Placement (2014, background): “Several studies proposed the optimum fiber path that minimizes the compliance of a cantilever beam [7], maximizes the buckling load of a plate [8], maximizes the buckling load of a hybrid composite shell [9], simultaneously maximizes the buckling load and in-plane stiffness [10].”