Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets

An aircraft wing needs to display different mechanical behavior in different directions. 1- stiffness in the spanwise (transverse to the corrugation) direction which enables the aerodynamic and inertial loads to be carried. 2- compliance in the chordwise (corrugation) direction which would allow sha...

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Main Authors: Pouyan Ghabezi, Mohammad Golzar
Format: Article
Language:fas
Published: Iran Polymer and Petrochemical Institute 2013-01-01
Series:علوم و تکنولوژی پلیمر
Subjects:
Online Access:http://jips.ippi.ac.ir/article_601_33de9848195061f5f990ee03bfe8730e.pdf
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author Pouyan Ghabezi
Mohammad Golzar
author_facet Pouyan Ghabezi
Mohammad Golzar
author_sort Pouyan Ghabezi
collection DOAJ
description An aircraft wing needs to display different mechanical behavior in different directions. 1- stiffness in the spanwise (transverse to the corrugation) direction which enables the aerodynamic and inertial loads to be carried. 2- compliance in the chordwise (corrugation) direction which would allow shape changes and increases in surface area; whereas a corrugated sheet due to their special geometry has potential to use in morphing applications. Therefore, in this paper the mechanical behaviour of quasi-sinusoidal corrugated composites is studied by commercial FEM software ABAQUS and a simple analytical model which is used for the initial stiffness of the quasi-sinusoidal corrugated composites (Yokozeki model). The elongation and effective stiffness in longitudinal and transverse directions of quasi-sinusoidal  corrugated  skins  and fat  composites  are  calculated  and  compared together.  Using  frst  and  second  Castigliano’s  theorem  and  Bernoulli-Euler  beam theorem can be used to calculate the defection and rotational angle of a beam (sheet). In this research, different dimensions of quasi-sinusoidal element for unidirectional and woven composites of E-glass/epoxy are investigated. FEM results and analytical model are compared together. Then, the analytical model is validated by experimental results of plain woven E-glass/epoxy composites. The results of FEM, experimental and analytical simulations show that how a corrugated composite can afford with certainty larger deformation than the fat composite in using this analytical model to predict the mechanical behavior of quasi-sinusoidal corrugated composites. It was found that the corrugated composites display extremely high anisotropic behavior and have high  tensile and fexural stiffness  in  transverse direction while exhibiting  low stiffness in longitudinal direction of corrugation.
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spelling doaj.art-f841f495274f48dda2fbfad48c10df3b2022-12-21T20:12:33ZfasIran Polymer and Petrochemical Instituteعلوم و تکنولوژی پلیمر1016-32552008-08832013-01-0124537938910.22063/jipst.2013.601601Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheetsPouyan GhabeziMohammad GolzarAn aircraft wing needs to display different mechanical behavior in different directions. 1- stiffness in the spanwise (transverse to the corrugation) direction which enables the aerodynamic and inertial loads to be carried. 2- compliance in the chordwise (corrugation) direction which would allow shape changes and increases in surface area; whereas a corrugated sheet due to their special geometry has potential to use in morphing applications. Therefore, in this paper the mechanical behaviour of quasi-sinusoidal corrugated composites is studied by commercial FEM software ABAQUS and a simple analytical model which is used for the initial stiffness of the quasi-sinusoidal corrugated composites (Yokozeki model). The elongation and effective stiffness in longitudinal and transverse directions of quasi-sinusoidal  corrugated  skins  and fat  composites  are  calculated  and  compared together.  Using  frst  and  second  Castigliano’s  theorem  and  Bernoulli-Euler  beam theorem can be used to calculate the defection and rotational angle of a beam (sheet). In this research, different dimensions of quasi-sinusoidal element for unidirectional and woven composites of E-glass/epoxy are investigated. FEM results and analytical model are compared together. Then, the analytical model is validated by experimental results of plain woven E-glass/epoxy composites. The results of FEM, experimental and analytical simulations show that how a corrugated composite can afford with certainty larger deformation than the fat composite in using this analytical model to predict the mechanical behavior of quasi-sinusoidal corrugated composites. It was found that the corrugated composites display extremely high anisotropic behavior and have high  tensile and fexural stiffness  in  transverse direction while exhibiting  low stiffness in longitudinal direction of corrugation.http://jips.ippi.ac.ir/article_601_33de9848195061f5f990ee03bfe8730e.pdffemmorphing technologyflexural and tensile stiffnesscompositequasi-sinusoidal corrugated sheets
spellingShingle Pouyan Ghabezi
Mohammad Golzar
Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets
علوم و تکنولوژی پلیمر
fem
morphing technology
flexural and tensile stiffness
composite
quasi-sinusoidal corrugated sheets
title Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets
title_full Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets
title_fullStr Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets
title_full_unstemmed Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets
title_short Mechanical Behavior of Quasi-sinusoidal Corrugated Composite sheets
title_sort mechanical behavior of quasi sinusoidal corrugated composite sheets
topic fem
morphing technology
flexural and tensile stiffness
composite
quasi-sinusoidal corrugated sheets
url http://jips.ippi.ac.ir/article_601_33de9848195061f5f990ee03bfe8730e.pdf
work_keys_str_mv AT pouyanghabezi mechanicalbehaviorofquasisinusoidalcorrugatedcompositesheets
AT mohammadgolzar mechanicalbehaviorofquasisinusoidalcorrugatedcompositesheets