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    Compressive Response and Failure of Circular Cell Polycarbonate Honeycombs Under Inplane Uniaxial Stresses 

    Source: Journal of Engineering Materials and Technology:;1999:;volume( 121 ):;issue: 004:;page 494
    Author(s): Jaeung Chung; Anthony M. Waas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The crushing response of polycarbonate circular cell honeycomb to inplane uniaxial loading under displacement control is analyzed through a combination of experiment and numerical simulation. The ...
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    In-Plane Biaxial Crush Response of Polycarbonate Honeycombs 

    Source: Journal of Engineering Mechanics:;2001:;Volume ( 127 ):;issue: 002
    Author(s): Jaeung Chung; Anthony M. Waas
    Publisher: American Society of Civil Engineers
    Abstract: The crushing response of a polycarbonate circular cell honeycomb to inplane biaxial loading under displacement control is analyzed. The study involves a combination of experiment and numerical simulation. Experiments ...
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    Global and Local Buckling of a Sandwich Beam 

    Source: Journal of Engineering Mechanics:;2007:;Volume ( 133 ):;issue: 002
    Author(s): Wooseok Ji; Anthony M. Waas
    Publisher: American Society of Civil Engineers
    Abstract: A two-dimensional mechanical model is developed to predict the global and local buckling of a sandwich beam, using classical elasticity. The face sheet and the core are assumed as linear elastic isotropic continua in a ...
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    Wrinkling and Edge Buckling in Orthotropic Sandwich Beams 

    Source: Journal of Engineering Mechanics:;2008:;Volume ( 134 ):;issue: 006
    Author(s): Wooseok Ji; Anthony M. Waas
    Publisher: American Society of Civil Engineers
    Abstract: A sandwich beam buckling problem is studied here using two-dimensional elasticity to model the beam constituents. The global and local instability of such a beam with orthotropic constituents under various boundary conditions ...
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    A Spring Foundation Model for Mode I Failure of Laminated Composites Based on an Energy Criterion 

    Source: Journal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 004:;page 512
    Author(s): Seung J. Song; Anthony M. Waas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A mechanical model which can predict mode I delamination failure of laminated composites has been developed. A beam on a nonlinear spring foundation was used to model experimental results ...
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    A Nondimensional Number to Classify Composite Compressive Failure 

    Source: Journal of Applied Mechanics:;2004:;volume( 071 ):;issue: 003:;page 402
    Author(s): Chandra S. Yerramalli; Anthony M. Waas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new nondimensional number (η) to predict the dominant failure mechanism of fiber reinforced composites under compression loading is presented. Results from previous experimental investigations ...
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    A Micromechanics-Based Finite Element Model for Compressive Failure of Notched Uniply Composite Laminates Under Remote Biaxial Loads 

    Source: Journal of Engineering Materials and Technology:;1999:;volume( 121 ):;issue: 003:;page 360
    Author(s): Jung H. Ahn; Anthony M. Waas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A micromechanics based failure initiation predictive capability for analyzing notched composite laminates loaded remotely in multiaxial compression is reported. The model relies on the results from ...
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    Convective Heat Transfer in Open Cell Metal Foams 

    Source: Journal of Heat Transfer:;2007:;volume( 129 ):;issue: 009:;page 1217
    Author(s): Ken I. Salas; Anthony M. Waas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Convective heat transfer in aluminum metal foam sandwich panels is investigated with potential applications to actively cooled thermal protection systems in hypersonic and re-entry vehicles. The ...
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    Experiments and Cohesive Zone Model Parameters for T650/AFR-PE-4/FM680-1 at High Temperatures 

    Source: Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003
    Author(s): Peter A. Gustafson; Anthony M. Waas
    Publisher: American Society of Civil Engineers
    Abstract: This paper reports an experimental program to establish a cohesive zone model for the T650/AFR-PE-4 (laminate) and FM680-1 (adhesive) system. The cohesive zone model is based on a four parameter characterization: in each ...
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    Buckling of Unilaterally Constrained Infinite Plates 

    Source: Journal of Engineering Mechanics:;1998:;Volume ( 124 ):;issue: 002
    Author(s): Khaled W. Shahwan; Anthony M. Waas
    Publisher: American Society of Civil Engineers
    Abstract: The problem of finding the buckling load of unilaterally constrained infinite plates is considered. The plates are modeled along the lines of classical plate theory employing Kirchhoff-Love hypotheses. The condition of ...
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