Search Results - "Littell, Justin"

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  1. 1

    Measurement of Epoxy Resin Tension, Compression, and Shear Stress–Strain Curves over a Wide Range of Strain Rates Using Small Test Specimens by Littell, Justin D, Ruggeri, Charles R, Goldberg, Robert K, Roberts, Gary D, Arnold, William A, Binienda, Wieslaw K

    Published in Journal of aerospace engineering (01-07-2008)
    “…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…”
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    Journal Article
  2. 2

    Effect of microscopic damage events on static and ballistic impact strength of triaxial braid composites by Littell, Justin D., Binienda, Wieslaw K., Arnold, William A., Roberts, Gary D., Goldberg, Robert K.

    “…The reliability of impact simulations for aircraft components made with triaxial braided carbon fiber composites is currently limited by inadequate material…”
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    Journal Article Conference Proceeding
  3. 3

    Characterization of Damage in Triaxial Braided Composites under Tensile Loading by Littell, Justin D, Binienda, Wieslaw K, Roberts, Gary D, Goldberg, Robert K

    Published in Journal of aerospace engineering (01-07-2009)
    “…Carbon fiber composites that utilize flattened, large tow yarns in woven or braided forms are being used in many aerospace applications. The complex fiber…”
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    Journal Article
  4. 4

    Methodology for Impact Modeling of Triaxial Braided Composites Using Shell Elements by Li, Xuetao, Binienda, Wieslaw K, Littell, Justin D

    Published in Journal of aerospace engineering (01-07-2009)
    “…In this paper, a two-dimensional triaxial braided composite model has been studied using the nonlinear explicit finite-element code LSDYNA. The unit cell…”
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    Journal Article
  5. 5

    Challenges in Vehicle Safety and Occupant Protection for Autonomous electric Vertical Take-off and Landing (eVTOL) Vehicles by Littell, Justin D.

    “…The burgeoning electric Vertical Take-off and Landing (eVTOL) vehicle industry has generated a significant level of enthusiasm amongst aviation designers,…”
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    Conference Proceeding
  6. 6

    Orion Crew Member Injury Predictions during Land and Water Landings by Lawrence, Charles, Littell, Justin D, Fasanella, Edwin L, Tabiei, Ala

    Published in Journal of aerospace engineering (01-07-2009)
    “…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…”
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    Journal Article
  7. 7

    Approximation of Nonlinear Unloading Effects in the Strain Rate Dependent Deformation Analysis of Polymer Matrix Materials Utilizing a State Variable Approach by Goldberg, Robert K, Roberts, Gary D, Littell, Justin D, Binienda, Wieslaw K

    Published in Journal of aerospace engineering (01-07-2008)
    “…An experimental and analytical program is carried out to explore key behaviors in the loading and unloading behavior of polymers. Specifically, the effects of…”
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    Journal Article
  8. 8

    Assessing biofidelity of the Test Device for Human Occupant Restraint (THOR) against historic human volunteer data by Newby, Nate, Somers, Jeffrey T, Caldwell, Erin E, Perry, Chris, Littell, Justin, Gernhardt, Michael

    Published in Stapp car crash journal (01-11-2013)
    “…The National Aeronautics and Space Administration (NASA) is interested in characterizing the responses of THOR (test device for human occupant restraint)…”
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    Journal Article
  9. 9

    The experimental and analytical characterization of the macromechanical response for triaxial braided composite materials by Littell, Justin

    Published 01-01-2008
    “…Increasingly, carbon composite structures are being used in aerospace applications. Due to their high strength, high stiffness and low weight properties, they…”
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    Dissertation
  10. 10

    The experimental and analytical characterization of the macromechanical response for triaxial braided composite materials by Littell, Justin

    “…Increasingly, carbon composite structures are being used in aerospace applications. Due to their high strength, high stiffness and low weight properties, they…”
    Get full text
    Dissertation