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    Methodology for Impact Modeling of Triaxial Braided Composites Using Shell Elements 

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003
    Author(s): Xuetao Li; Wieslaw K. Binienda; Justin D. Littell
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, a two-dimensional triaxial braided composite model has been studied using the nonlinear explicit finite-element code LSDYNA. The unit cell consists of six subcells and material properties associated with ...
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    Orion Crew Member Injury Predictions during Land and Water Landings 

    Source: Journal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 003
    Author(s): Charles Lawrence; Justin D. Littell; Edwin L. Fasanella; Ala Tabiei
    Publisher: American Society of Civil Engineers
    Abstract: A review of astronaut whole body impact tolerance is discussed for land or water landings of the next generation manned space capsule named Orion. LS-DYNA simulations of Orion capsule landings are performed to produce a ...
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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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    Measurement of Epoxy Resin Tension, Compression, and Shear Stress–Strain Curves over a Wide Range of Strain Rates Using Small Test Specimens 

    Source: Journal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 003
    Author(s): Justin D. Littell; Charles R. Ruggeri; Robert K. Goldberg; Gary D. Roberts; William A. Arnold; Wieslaw K. Binienda
    Publisher: American Society of Civil Engineers
    Abstract: The next generation aircraft engines are designed to be lighter and stronger than engines currently in use by using carbon fiber composites. In order to certify these engines, ballistic impact tests and computational ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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