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摘要:
The study of stratospheric airships has become the focus in many countries in recent years,because of its potential applications in many fields.Lightweight and high strength envelopes are the keys to the design of stratospheric airships,as it directly determines the endurance flight performance and loading deformation characteristics of the airship.A typical envelope of any stratospheric airship is a coated-fabric material which is composed of a fiber layer and several functional membrane layers.According to composite structure,nonlinearity and viscoelasticity are the two main characteristics of such envelope.Based on the analysis on the interaction between the different components in the micro-mechanical model of the coated-fabric,several invariant values reflecting the characteristics of the envelope material are obtained according to invariant theory.Furthermore,the constitutive equation that describes the viscoelasticity of the envelope material is derived.The constitutive equation can represent both the individual roles of the warp and weft fibers,and their further coupled interactions.The theoretical computation results were verified by off-axial tension tests.The results can help gain a deeper understanding of the mechanical mechanism and provide a reference for structural design of envelope material.
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篇名 The Constitutive Relation of a Fabric Membrane Composite for a Stratospheric Airship Envelope Based on Invariant Theory
来源期刊 计算机、材料和连续体(英文) 学科 数学
关键词 STRATOSPHERIC AIRSHIP FABRIC MEMBRANE COMPOSITE CONSTITUTIVE relation invariant theory viscoelasticity.
年,卷(期) 2017,(2) 所属期刊栏目
研究方向 页码范围 73-89
页数 17页 分类号 O17
字数 语种
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研究主题发展历程
节点文献
STRATOSPHERIC
AIRSHIP
FABRIC
MEMBRANE
COMPOSITE
CONSTITUTIVE
relation
invariant
theory
viscoelasticity.
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研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
计算机、材料和连续体(英文)
月刊
1546-2218
江苏省南京市浦口区东大路2号东大科技园A
出版文献量(篇)
346
总下载数(次)
4
总被引数(次)
0
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