Two-level composite wing structural optimization using response surfaces
By B. Liu, Raphael T. Haftka, M. Akgün. 2000
143 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Civil and Structural Engineering, Computational Theory and Mathematics
View Paper: https://www.semanticscholar.org/paper/cfaa5640656cba956bb83d7532219dee8369248e
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
- Kazem Fayazbakhsh
- Damiano Pasini
- L. Lessard
- Sondipon Adhikari
- Boyang Liu
- Layne T. Watson
- Tanmoy Mukhopadhyay
- S. Dey
In Civil and Structural Engineering
- Tanmoy Mukhopadhyay
- S. Dey
- Sondipon Adhikari
- Kazem Fayazbakhsh
- Damiano Pasini
- L. Lessard
- Hossein Ghiasi
- Boyang Liu
In Computational Theory and Mathematics
- Sondipon Adhikari
- Tanmoy Mukhopadhyay
- S. Dey
- Boyang Liu
- Layne T. Watson
- Damiano Pasini
- Raphael T. Haftka
- Hossein Ghiasi
Citations in the corpus
- Metamodel based high-fidelity stochastic analysis of composite laminates: A concise review with critical comparative assessment (2017, methodology): “[32] used a cubic response surface combined with a twolevel optimization technique to maximize the buckling load of a composite wing.”
- Global-local structural optimization using response surfaces of local optimization margins (2004, methodology): “A special version of this approach was developed for coordinating panel design with overall wing design by Liu et al. (2000).”
- Optimum stacking sequence design of composite materials Part II: Variable stiffness design (2010, methodology): “[57] minimized the weight of a wing structure using continuous optimization of thicknesses of four plies with orientations of 0 , 90 , and ±45 , at the upper level.”