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    Analytical Solution for Flexural Response of Epoxy Resin Materials

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003
    Author:
    Masoud Yekani Fard
    ,
    Yingtao Liu
    ,
    Aditi Chattopadhyay
    DOI: 10.1061/(ASCE)AS.1943-5525.0000133
    Publisher: American Society of Civil Engineers
    Abstract: A piecewise linear parametric uniaxial stress-strain approach has been used to obtain the closed form nonlinear moment curvature response on the basis of strain compatibility in bending for epoxy resin materials. The stress-strain curves, consisting of a bilinear ascending curve followed by strain softening and constant plastic flow in tension and compression, are described by two main parameters, with an additional five nondimensional tensile and seven nondimensional compressive parameters. The main parameters are the modulus of elasticity and strain at the proportional elastic limit point in tension. Parametric studies show that ultimate tensile stress and compressive yield stresses and tension and compression flow stresses have the highest effects on flexural load carrying capacity. Moment curvature equations, in conjunction with softening localization and static equilibrium conditions, were used to simulate the flexural load-deflection response of a beam under three-point bending (3PB) conditions. The simulations and experiments reveal that the direct use of uniaxial tensile and compressive stress-strain curves underestimates the flexural response caused by the stress gradient and the differences in the effective volume of the body subjected to critical stresses.
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      Analytical Solution for Flexural Response of Epoxy Resin Materials

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/56278
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    • Journal of Aerospace Engineering

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    contributor authorMasoud Yekani Fard
    contributor authorYingtao Liu
    contributor authorAditi Chattopadhyay
    date accessioned2017-05-08T21:33:51Z
    date available2017-05-08T21:33:51Z
    date copyrightJuly 2012
    date issued2012
    identifier other%28asce%29as%2E1943-5525%2E0000133.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56278
    description abstractA piecewise linear parametric uniaxial stress-strain approach has been used to obtain the closed form nonlinear moment curvature response on the basis of strain compatibility in bending for epoxy resin materials. The stress-strain curves, consisting of a bilinear ascending curve followed by strain softening and constant plastic flow in tension and compression, are described by two main parameters, with an additional five nondimensional tensile and seven nondimensional compressive parameters. The main parameters are the modulus of elasticity and strain at the proportional elastic limit point in tension. Parametric studies show that ultimate tensile stress and compressive yield stresses and tension and compression flow stresses have the highest effects on flexural load carrying capacity. Moment curvature equations, in conjunction with softening localization and static equilibrium conditions, were used to simulate the flexural load-deflection response of a beam under three-point bending (3PB) conditions. The simulations and experiments reveal that the direct use of uniaxial tensile and compressive stress-strain curves underestimates the flexural response caused by the stress gradient and the differences in the effective volume of the body subjected to critical stresses.
    publisherAmerican Society of Civil Engineers
    titleAnalytical Solution for Flexural Response of Epoxy Resin Materials
    typeJournal Paper
    journal volume25
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000133
    treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003
    contenttypeFulltext
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