J Sun, Q Guan, Y Liu, J Leng - Journal of Intelligent material …, 2016 - journals.sagepub.com
A traditional aircraft is optimized for only one or two flight conditions, not for the entire flight envelope. In contrast, the wings of a bird can be reshaped to provide optimal performance at …
ZZ Wang, A Sobey - Composite Structures, 2020 - Elsevier
The task of providing optimal composite structures is increasingly difficult. New analysis approaches seek to model the material at the fibre/matrix scale and increasingly more …
Corrugation has long been seen as a simple and effective means of forming lightweight structures with high anisotropic behaviour, stability under buckling load and energy …
Considering that from 1981 up to 2016 there was a 220% increase in aircraft production, due to the increased by 4.7% Compound Annual Growth Rate (CAGR) of travel demand, we …
In the present study, a novel theoretical model is developed, based on the energy method, to predict the equivalent mechanical properties of a new morphing structure with zero …
This paper deals with the buckling behavior of corrugated thin plates made of multilayer functionally graded (FG) graphene nanoplatelets (GPLs) reinforced nanocomposites (FG …
KJ Park, K Jung, YW Kim - Composite Structures, 2016 - Elsevier
Corrugated panels are widely used as structural elements in engineering fields because of their high stiffness and light weight. Moreover, corrugated composite laminates have …
A Jha, I Dayyani - Composite Structures, 2021 - Elsevier
This article investigates the potential of a large strain morphing skin based on a Zero Poisson's Ratio (ZPR) Fish-Cells metamaterial. A multi-objective genetic algorithm shape …
G Cheng, L Xu - Structural and Multidisciplinary Optimization, 2016 - Springer
This paper studies maximum out-of-plane buckling load design of thin bending plates for a given amount of material. Two kinds of plates are considered. One is made of periodic …