Optimum design of aircraft panels based on adaptive dynamic harmony search-Reference-Cited by-同舟云学术

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Optimum design of aircraft panels based on adaptive dynamic harmony search

Published:2017-09 Issue: Volume:118 Page:37-45
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Keshtegar Behrooz,Hao Peng,Wang Yutian,Li Yangfan

Funder

National Natural Science Foundation of China

University of Zabol

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference47 articles.

1. Buckling behavior of compression-loaded quasi-isotropic curved panels with a circular cutout;Hilburger;Int. J. Solids Struct.,2001

2. Optimization of fiber orientations near a hole for increased load-carrying capacity of composite laminates;Huang;Struct. Multidiscip. Optim.,2005

3. Future structural stability design for composite space and airframe structures;Degenhardt;Thin-Walled Struct.,2014

4. Buckling of axially compressed CFRP truncated cones with additional lateral load: experimental and numerical investigation;Khakimova;Compos. Struct.,2016

5. Integrated optimization of hybrid-stiffness stiffened shells based on sub-panel elements;Hao;Thin-Walled Struct.,2016

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