Multiobjective optimization of laminated composite cylindrical shells for maximum frequency and buckling load
By U. Topal. 2009
66 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Civil and Structural Engineering, Mechanics of Materials
View Paper: https://www.semanticscholar.org/paper/254dc6795be93054dd281f61ce9675cbc024ff3e
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
In Civil and Structural Engineering
- G. Nie
- Esben Lindgaard
- Romesh C. Batra
- Erik Lund
- Ashraf M. Zenkour
- Erasmo Carrera
- K. Swaminathan
- L. Qian
In Mechanics of Materials
- G. Nie
- Romesh C. Batra
- Esben Lindgaard
- Erik Lund
- Erasmo Carrera
- K. Swaminathan
- Salvatore Brischetto
- Ashraf M. Zenkour
Citations in the corpus
- Material tailoring and analysis of functionally graded isotropic and incompressible linear elastic hollow cylinders (2010, background): “Optimization problems involving more than one variable to be optimized have been studied, for example, in [27,28].”
- Optimization formulations for the maximum nonlinear buckling load of composite structures (2011, background): “…(1992); Walker et al (1996); Mateus et al (1997); Walker (2001); Foldager et al (2001); Hu and Yang (2007); Topal and Uzman (2008); Lund (2009); Topal (2009), have considered buckling optimization of composite structures where the buckling load was determined by the solution to the linearized…”