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    Influence of Load Type and Stress Gradient on Flexural Strength of Epoxy Resin Polymeric Material

    Source: Journal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 001
    Author:
    Masoud
    ,
    Yekani Fard
    ,
    Aditi
    ,
    Chattopadhyay
    ,
    Yingtao
    ,
    Liu
    DOI: 10.1061/(ASCE)AS.1943-5525.0000228
    Publisher: American Society of Civil Engineers
    Abstract: A piecewise-linear parametric uniaxial stress-strain approach has been used to obtain the nonlinear moment curvature response based on strain compatibility in bending for epoxy resin materials. It has been shown that the direct use of tension and compression stress-strain models underestimates the flexural strength of epoxy resin materials in a three-point bending (3PB) setup. An analytical and experimental investigation is conducted to better evaluate the degree of flexural overstrength for epoxy resin material. Four-point bending (4PB) and a round plate (RP) supported on three symmetrically arranged pivot points on a circle are chosen. An algorithm is developed to obtain the load-deflection response of the 4PB and RP samples from the nonlinear moment curvature curve. Small-sized 3PB tests are conducted to examine the size effects on the flexural response. The experimental nonlinear load-deflection responses obtained in the various load arrangements are satisfactorily simulated through the developed algorithm. The simulations and experiments reveal that the ratio of the experimental flexural strength to that obtained through simulation (flexural overstrength factor) in 4PB is higher than the corresponding values in 3PB and the round panel. The conservative value of 1.14 could be used as the flexural overstrength factor for epoxy resin materials in analysis and design.
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      Influence of Load Type and Stress Gradient on Flexural Strength of Epoxy Resin Polymeric Material

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56380
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    contributor authorMasoud
    contributor authorYekani Fard
    contributor authorAditi
    contributor authorChattopadhyay
    contributor authorYingtao
    contributor authorLiu
    date accessioned2017-05-08T21:34:02Z
    date available2017-05-08T21:34:02Z
    date copyrightJanuary 2014
    date issued2014
    identifier other%28asce%29as%2E1943-5525%2E0000228.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56380
    description abstractA piecewise-linear parametric uniaxial stress-strain approach has been used to obtain the nonlinear moment curvature response based on strain compatibility in bending for epoxy resin materials. It has been shown that the direct use of tension and compression stress-strain models underestimates the flexural strength of epoxy resin materials in a three-point bending (3PB) setup. An analytical and experimental investigation is conducted to better evaluate the degree of flexural overstrength for epoxy resin material. Four-point bending (4PB) and a round plate (RP) supported on three symmetrically arranged pivot points on a circle are chosen. An algorithm is developed to obtain the load-deflection response of the 4PB and RP samples from the nonlinear moment curvature curve. Small-sized 3PB tests are conducted to examine the size effects on the flexural response. The experimental nonlinear load-deflection responses obtained in the various load arrangements are satisfactorily simulated through the developed algorithm. The simulations and experiments reveal that the ratio of the experimental flexural strength to that obtained through simulation (flexural overstrength factor) in 4PB is higher than the corresponding values in 3PB and the round panel. The conservative value of 1.14 could be used as the flexural overstrength factor for epoxy resin materials in analysis and design.
    publisherAmerican Society of Civil Engineers
    titleInfluence of Load Type and Stress Gradient on Flexural Strength of Epoxy Resin Polymeric Material
    typeJournal Paper
    journal volume27
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000228
    treeJournal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 001
    contenttypeFulltext
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