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  1. National Taiwan Ocean University Research Hub

Nonlinear Viscoelastic Analysis of FRP Laminated Plates and Shells

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基本資料

Project title
Nonlinear Viscoelastic Analysis of FRP Laminated Plates and Shells
Code/計畫編號
NSC88-2212-E019-005
Translated Name/計畫中文名
纖維強化塑膠積層板殼之非線性黏彈分析
 
Project Coordinator/計畫主持人
Nan-Nong Huang
Funding Organization/主管機關
National Science and Technology Council
 
Department/Unit
Department of Mechanical and Mechatronic Engineering
Website
https://www.grb.gov.tw/search/planDetail?id=418783
Year
1999
 
Start date/計畫起
01-08-1998
Expected Completion/計畫迄
01-07-1999
 
Bugetid/研究經費
125千元
 
ResearchField/研究領域
機械工程
 

Description

Abstract
本研究主要在於探討承受壓力之纖維強化塑膠基層板之潛變挫曲及潛變大撓度變形。考慮材料非線性及幾何缺陷對於結構黏彈反應之影響。複合材料非線性黏彈應變-應力關係是採用Schapery單迴旋積分式來描述。文中詳細探討對稱正交積層板承受軸向壓力所衍生之結構潛變行為。使用的板理論為古典積層板理論,並引入von Karman撓性板假設。利用虛功原理求取約略解。為簡化分析程序及節省數值計算時間,本研究採用準彈性分析。 The objective of this research is to investigate the creep buckling and large creep deflection of fiber-reinforced-plastic (FRP) laminated plates under compression. The effects of material nonlinearity and geometrical imperfection on the viscoelastic behaviors are examined. The nonlinear viscoelastic strain-stress relation is described by Schapery's single- convolution- integral constitutive law. The creep responses of symmetric cross-ply laminates subjected to the in-plane axial compression are thorough investigated and reported in this study. The analysis is based on the classicallaminate theory in conjunction with the von Karman flexible plate hypothesis. The approximate solutions are obtained using the principle of virtual work. In order to simplify the analysis procedure and improve the numerical computation efficiency, the quasi-elastic approach is adopted in this study.
 
Keyword(s)
纖維強化塑膠
積層板
非線性黏彈
幾何不完全潛變挫曲
有限元素法
單迴旋積分
Fiber reinforced plastic (FRP)
Laminated plate
Nonlinear viscoelasticity
Geometrical imperfection creep buckling
Finite element method (FEM)
Single convolution integral
 
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