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    Design and Testing of an Airbag System for High-Mass, High-Velocity Deceleration

    Source: Journal of Dynamic Systems, Measurement, and Control:;1997:;volume( 119 ):;issue: 004::page 631
    Author:
    T. Snyder
    ,
    J. Sitter
    ,
    J. N. Chung
    DOI: 10.1115/1.2802371
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design and performance evaluation of an airbag system capable of decelerating masses in the range of hundreds to thousands of kilograms with impact velocities in the range of tens to hundreds of kilometers per hour is presented. First, a simplified incompressible flow analysis of the airbag is utilized to derive the orifice venting area corresponding to the ideal deceleration for a given impact velocity and package mass. Second, testing with a small-scale model found three distinct control intervals during the deceleration. Finally, a full-scale airbag system was constructed and data is presented on the deceleration, deceleration force, deceleration velocity, airbag stopping power, and overall performance. The deceleration was experimentally optimized for a single impact velocity and package mass and an approximate correction factor was developed to predict the actual air venting required for each of the three control intervals in order to achieve the optimum deceleration for any impact velocity and package mass.
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      Design and Testing of an Airbag System for High-Mass, High-Velocity Deceleration

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/118359
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    • Journal of Dynamic Systems, Measurement, and Control

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    contributor authorT. Snyder
    contributor authorJ. Sitter
    contributor authorJ. N. Chung
    date accessioned2017-05-08T23:52:52Z
    date available2017-05-08T23:52:52Z
    date copyrightDecember, 1997
    date issued1997
    identifier issn0022-0434
    identifier otherJDSMAA-26241#631_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118359
    description abstractThe design and performance evaluation of an airbag system capable of decelerating masses in the range of hundreds to thousands of kilograms with impact velocities in the range of tens to hundreds of kilometers per hour is presented. First, a simplified incompressible flow analysis of the airbag is utilized to derive the orifice venting area corresponding to the ideal deceleration for a given impact velocity and package mass. Second, testing with a small-scale model found three distinct control intervals during the deceleration. Finally, a full-scale airbag system was constructed and data is presented on the deceleration, deceleration force, deceleration velocity, airbag stopping power, and overall performance. The deceleration was experimentally optimized for a single impact velocity and package mass and an approximate correction factor was developed to predict the actual air venting required for each of the three control intervals in order to achieve the optimum deceleration for any impact velocity and package mass.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign and Testing of an Airbag System for High-Mass, High-Velocity Deceleration
    typeJournal Paper
    journal volume119
    journal issue4
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.2802371
    journal fristpage631
    journal lastpage637
    identifier eissn1528-9028
    treeJournal of Dynamic Systems, Measurement, and Control:;1997:;volume( 119 ):;issue: 004
    contenttypeFulltext
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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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