Scale Models for Laminated Cylindrical Shells Subjected to Axial Compression
سال
: 1996
چکیده: This study investigates problems associated with the design of scaled down
models. Such study is important since it provides the necessary scaling laws,
and the factors which affect the accuracy of the scale models. For better
understanding the applicability of scaled down models in designing
laminated composite structures, an analytical investigation was undertaken
to assess the feasibility of their use. Employment of similitude theory to
establish similarity among structurai systems can save considerable expense
and time, provided that the proper scaling laws are found and validated. In
this study the limitation and acceptable interval of all parameters and
corresponding scale factors are investigated. Particular emphasis is placed
on the case of buckling of cross-ply cylindrical shells under uniaxial
compressive loads. Both complete and partial similarity are discussed. This
analytical study indicates that distorted models with a different number of
layers and geometries than those of the prototype can predict the behavior
of the prototype with good accuracy. However, it is shown that a scaled
down model with different material properties than those of the prototype
is incapable of predicting the response of the prototype.
models. Such study is important since it provides the necessary scaling laws,
and the factors which affect the accuracy of the scale models. For better
understanding the applicability of scaled down models in designing
laminated composite structures, an analytical investigation was undertaken
to assess the feasibility of their use. Employment of similitude theory to
establish similarity among structurai systems can save considerable expense
and time, provided that the proper scaling laws are found and validated. In
this study the limitation and acceptable interval of all parameters and
corresponding scale factors are investigated. Particular emphasis is placed
on the case of buckling of cross-ply cylindrical shells under uniaxial
compressive loads. Both complete and partial similarity are discussed. This
analytical study indicates that distorted models with a different number of
layers and geometries than those of the prototype can predict the behavior
of the prototype with good accuracy. However, it is shown that a scaled
down model with different material properties than those of the prototype
is incapable of predicting the response of the prototype.
کلیدواژه(گان): Scale Model,Laminated,Cylindrical Shells,Axial Compression
کالکشن
:
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آمار بازدید
Scale Models for Laminated Cylindrical Shells Subjected to Axial Compression
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contributor author | جلیل رضائی پژند | en |
contributor author | G. J. Simitses | en |
contributor author | J. H. Starnes Jr | en |
contributor author | Jalil Rezaee Pazhand | fa |
date accessioned | 2020-06-06T13:06:52Z | |
date available | 2020-06-06T13:06:52Z | |
date issued | 1996 | |
identifier uri | http://libsearch.um.ac.ir:80/fum/handle/fum/3342122 | |
description abstract | This study investigates problems associated with the design of scaled down models. Such study is important since it provides the necessary scaling laws, and the factors which affect the accuracy of the scale models. For better understanding the applicability of scaled down models in designing laminated composite structures, an analytical investigation was undertaken to assess the feasibility of their use. Employment of similitude theory to establish similarity among structurai systems can save considerable expense and time, provided that the proper scaling laws are found and validated. In this study the limitation and acceptable interval of all parameters and corresponding scale factors are investigated. Particular emphasis is placed on the case of buckling of cross-ply cylindrical shells under uniaxial compressive loads. Both complete and partial similarity are discussed. This analytical study indicates that distorted models with a different number of layers and geometries than those of the prototype can predict the behavior of the prototype with good accuracy. However, it is shown that a scaled down model with different material properties than those of the prototype is incapable of predicting the response of the prototype. | en |
language | English | |
title | Scale Models for Laminated Cylindrical Shells Subjected to Axial Compression | en |
type | Journal Paper | |
contenttype | External Fulltext | |
subject keywords | Scale Model | en |
subject keywords | Laminated | en |
subject keywords | Cylindrical Shells | en |
subject keywords | Axial Compression | en |
journal title | Composite Structures | en |
journal title | Composite Structures | fa |
pages | 371-379 | |
journal volume | 34 | |
journal issue | 4 | |
identifier link | https://profdoc.um.ac.ir/paper-abstract-1026096.html | |
identifier articleid | 1026096 |