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    Failure Model for Rate-Dependent Polymer Matrix Composite Laminates under High-Velocity Impact 

    Source: Journal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 003
    Author(s): Linfa Zhu; Aditi Chattopadhyay; Robert K. Goldberg
    Publisher: American Society of Civil Engineers
    Abstract: A modified Hashin failure model is developed to characterize different failure modes related to high-velocity impact of composite laminates. Hashin’s compressive fiber failure mode has been extended to consider the shear ...
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    Ballistic Impact and Crashworthiness Response of Aerospace Structures 

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003
    Author(s): Robert K. Goldberg; Wieslaw K. Binienda
    Publisher: American Society of Civil Engineers
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    Dynamic Testing and Characterization of Woven/Braided Polymer Composites: A Review 

    Source: Applied Mechanics Reviews:;2011:;volume( 064 ):;issue: 005:;page 50803
    Author(s): Wieslaw K. Binienda; Robert K. Goldberg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Woven and braided polymer composite structures are used in many primary aerospace applications because of their superior behavior under dynamic loading conditions and light weight. Characterization ...
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    Implementation of an Associative Flow Rule Including Hydrostatic Stress Effects into the High Strain Rate Deformation Analysis of Polymer Matrix Composites 

    Source: Journal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 001
    Author(s): Robert K. Goldberg; Gary D. Roberts; Amos Gilat
    Publisher: American Society of Civil Engineers
    Abstract: A previously developed analytical formulation has been modified in order to more accurately account for the effects of hydrostatic stresses on the nonlinear, strain rate dependent deformation of polymer matrix composites. ...
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    Strain Rate Sensitivity of Epoxy Resin in Tensile and Shear Loading 

    Source: Journal of Aerospace Engineering:;2007:;Volume ( 020 ):;issue: 002
    Author(s): Amos Gilat; Robert K. Goldberg; Gary D. Roberts
    Publisher: American Society of Civil Engineers
    Abstract: The mechanical response of E-862 and PR-520 resins is investigated in tensile and shear loadings. At both types of loading the resins are tested at strain rates of about
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    Finite-Element Model for Failure Study of Two-Dimensional Triaxially Braided Composite 

    Source: Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 002
    Author(s): Xuetao Li; Wieslaw K. Binienda; Robert K. Goldberg
    Publisher: American Society of Civil Engineers
    Abstract: A new three-dimensional finite-element model of two-dimensional, triaxially braided composites is presented in this paper. This mesoscale modeling technique is used to examine and predict the deformation and damage observed ...
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    Modification of a Macromechanical Finite Element–Based Model for Impact Analysis of Triaxially Braided Composites 

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003
    Author(s): Robert K. Goldberg; Brina J. Blinzler; Wieslaw K. Binienda
    Publisher: American Society of Civil Engineers
    Abstract: A macrolevel finite element–based model has been developed to simulate the mechanical and impact response of triaxially braided polymer matrix composites. In the analytical model, the triaxial-braid architecture is simulated ...
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    Approximation of Nonlinear Unloading Effects in the Strain Rate Dependent Deformation Analysis of Polymer Matrix Materials Utilizing a State Variable Approach 

    Source: Journal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 003
    Author(s): Robert K. Goldberg; Gary D. Roberts; Justin D. Littell; Wieslaw K. Binienda
    Publisher: American Society of Civil Engineers
    Abstract: An experimental and analytical program is carried out to explore key behaviors in the loading and unloading behavior of polymers. Specifically, the effects of strain rate and hydrostatic stresses on the nonlinear portions ...
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    Characterization of Damage in Triaxial Braided Composites under Tensile Loading 

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003
    Author(s): Justin D. Littell; Wieslaw K. Binienda; Gary D. Roberts; Robert K. Goldberg
    Publisher: American Society of Civil Engineers
    Abstract: Carbon fiber composites that utilize flattened, large tow yarns in woven or braided forms are being used in many aerospace applications. The complex fiber architecture and large unit cell size in these materials present ...
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    Single Ply and Multi-Ply Braided Composite Response Predictions Using Modified Subcell Approach 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 005
    Author(s): Christopher R. Cater; Xinran Xiao; Robert K. Goldberg; Lee. W. Kohlman
    Publisher: American Society of Civil Engineers
    Abstract: In this work, the modeling of triaxially braided composites was explored through a subcell approach using an improved semianalytical discretization scheme. The unit cell of the braided composite was divided into four unique ...
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