Optimization of Variable-Stiffness Panels for Maximum Buckling Load Using Lamination Parameters
By Samuel T. IJsselmuiden, Mostafa Abdalla, Zafer Gürdal. 2010
208 citations recorded by the source corpus.
Subfields: Civil and Structural Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/24cab9ccd6c577d793b7aacbbfe3c6a586dfdf71
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
- M. A. Nik
- L. Lessard
- Damiano Pasini
- Tanmoy Mukhopadhyay
- S. Dey
- Sondipon Adhikari
- Marco Montemurro
In Mechanics of Materials
- Kazem Fayazbakhsh
- M. A. Nik
- Damiano Pasini
- L. Lessard
- Tanmoy Mukhopadhyay
- Sondipon Adhikari
- S. Dey
- Joris Degrieck
Citations in the corpus
- Stiffness Optimization of Composite Wings with Aeroelastic Constraints (2012, unknown): “[14].”
- Framework for the Buckling Optimization of Variable-Angle Tow Composite Plates (2015, unknown): “[5,15] presented a sophisticated framework based on finite element modeling and a successive approximation optimization technique [16] to perform the design of variable stiffness structures for maximum buckling load.”
- Surrogate-based multi-objective optimization of a composite laminate with curvilinear fibers (2012, background): “[8] studied different loading and boundary conditions on balanced symmetric [±h]3s square plates.”