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    Inertial Loading of the Human Cervical Spine

    Source: Journal of Biomechanical Engineering:;1997:;volume( 119 ):;issue: 003::page 237
    Author:
    N. Yoganandan
    ,
    F. A. Pintar
    DOI: 10.1115/1.2796086
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: While the majority of experimental cervical spine biomechanics research has been conducted using slowly applied forces and/or moments, or dynamically applied forces with contact, little research has been performed to delineate the biomechanics of the human neck under inertial “noncontact” type forces. This study was designed to develop a comprehensive methodology to induce these loads. A minisled pendulum experimental setup was designed to test specimens (such as human cadaver neck) at subfailure or failure levels under different loading modalities including flexion, extension, and lateral bending. The system allows acceleration/deceleration input with varying wave form shapes. The test setup dynamically records the input and output strength information such as forces, accelerations, moments, and angular velocities; it also has the flexibility to obtain the temporal overall and local kinematic data of the cervical spine components at every vertebral level. These data will permit a complete biomechanical structural analysis. In this paper, the feasibility of the methodology is demonstrated by subjecting a human cadaver head-neck complex with intact musculature and skin under inertial flexion and extension whiplash loading at two velocities.
    keyword(s): Cervical spine , Force , Biomechanics , Waves , Failure , Muscle , Pendulums , Shapes , Skin , Plasticity , Structural analysis AND Stress ,
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      Inertial Loading of the Human Cervical Spine

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    contributor authorN. Yoganandan
    contributor authorF. A. Pintar
    date accessioned2017-05-08T23:52:46Z
    date available2017-05-08T23:52:46Z
    date copyrightAugust, 1997
    date issued1997
    identifier issn0148-0731
    identifier otherJBENDY-25976#237_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118293
    description abstractWhile the majority of experimental cervical spine biomechanics research has been conducted using slowly applied forces and/or moments, or dynamically applied forces with contact, little research has been performed to delineate the biomechanics of the human neck under inertial “noncontact” type forces. This study was designed to develop a comprehensive methodology to induce these loads. A minisled pendulum experimental setup was designed to test specimens (such as human cadaver neck) at subfailure or failure levels under different loading modalities including flexion, extension, and lateral bending. The system allows acceleration/deceleration input with varying wave form shapes. The test setup dynamically records the input and output strength information such as forces, accelerations, moments, and angular velocities; it also has the flexibility to obtain the temporal overall and local kinematic data of the cervical spine components at every vertebral level. These data will permit a complete biomechanical structural analysis. In this paper, the feasibility of the methodology is demonstrated by subjecting a human cadaver head-neck complex with intact musculature and skin under inertial flexion and extension whiplash loading at two velocities.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInertial Loading of the Human Cervical Spine
    typeJournal Paper
    journal volume119
    journal issue3
    journal titleJournal of Biomechanical Engineering
    identifier doi10.1115/1.2796086
    journal fristpage237
    journal lastpage240
    identifier eissn1528-8951
    keywordsCervical spine
    keywordsForce
    keywordsBiomechanics
    keywordsWaves
    keywordsFailure
    keywordsMuscle
    keywordsPendulums
    keywordsShapes
    keywordsSkin
    keywordsPlasticity
    keywordsStructural analysis AND Stress
    treeJournal of Biomechanical Engineering:;1997:;volume( 119 ):;issue: 003
    contenttypeFulltext
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