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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.03.025
Abstract: Abstract In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the static nonlinear aeroelastic response of morphing composite wing with orthotropic materials has been developed. A flat plate/shell finite element, which can model…
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Keywords:
static aeroelastic;
geometrically nonlinear;
wing;
model ... See more keywords
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Published in 2020 at "Composite Structures"
DOI: 10.1016/j.compstruct.2020.112370
Abstract: Abstract In this article, the energy absorption capability and crushing behavior of composite corrugated tubes have been studied experimentally and numerically under quasi-static axial slipping crushing loading. Five corrugations with angles ranging between 35° and…
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Keywords:
cfrp kfrp;
composite corrugated;
quasi static;
corrugated tubes ... See more keywords
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Published in 2020 at "Composite Structures"
DOI: 10.1016/j.compstruct.2020.112996
Abstract: Abstract Due to the versatility of load bearing and heat insulation, foam-filled composite corrugated sandwich plates have a broad application in aerospace industry as thermal insulation structures for hypersonic vehicles. In this paper, a C0…
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Keywords:
composite corrugated;
order;
filled composite;
model ... See more keywords
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Published in 2021 at "Thin-walled Structures"
DOI: 10.1016/j.tws.2020.107157
Abstract: Abstract This article describes an experimental study of the impact behaviour of a novel composite corrugated core sandwich structure under low-velocity impact. Influences of geometric parameters of the novel sandwich core, such as thickness, height,…
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Keywords:
composite corrugated;
low velocity;
impact;
velocity impact ... See more keywords