YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Vibration and Acoustics
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Vibration and Acoustics
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Study of Far Field Pyroshock Responses of Composite Panels

    Source: Journal of Vibration and Acoustics:;2014:;volume( 136 ):;issue: 003::page 31014
    Author:
    Velmurugan, R.
    ,
    Mohamed Najeeb, E.
    DOI: 10.1115/1.4027223
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The experimental and numerical studies on farfield pyroshock responses of composite panels are presented in this paper. The purpose of this study is to find out the region of composite panel where the pyroshock response is high and thereby the panel can be used as a testing bed to examine tiny elements such as electronic parts used in spacecraft. Experiments based on biplate technology are conducted on different combination of eglass/epoxy composite panel parameters. The structural responses are analyzed using panel parameters as well as shock response spectrums (SRSs) computed from the accelerationtime histories. The experiments are carried out for a low range of chamber pressure with projectiles of varying length to get the farfield response of the test panel. The accelerations of the panel at selected locations are measured by the PCB Piezotronics (Depew, NY) accelerometers and National InstrumentsData Acquisition (NIDAQ) system (National Instruments, Austin, TX) with labview software. Finite element analysis (FEA) for the pyroshock environment is done using abaqus/Explicit software. Due to the symmetry of the structure as well as the loading, only quarter portion of the panel is analyzed. From the results, it is found that acceleration increases as thickness of composite test panel increases (about 20–70%) for all the combinations of projectile length and chamber pressure at all the points considered on the laminate. Transfer of acceleration from steel plate onto composite panel through physical connections is predominant (about 90–95% of total transfer) than that through air media between the steel plate and the composite panel. Velocity with lower momentum induces lower frequency modes to be dominant whereas velocity with higher momentum induces higher frequency modes. Normally higher accelerations (about 40–90%) are experienced at the center location than any other locations under consideration. The SRSs are obtained both from FEA and experiments. The experimental study shows good agreement with the FEA results both in acceleration time history as well as in SRS.
    • Download: (3.414Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Study of Far Field Pyroshock Responses of Composite Panels

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/156762
    Collections
    • Journal of Vibration and Acoustics

    Show full item record

    contributor authorVelmurugan, R.
    contributor authorMohamed Najeeb, E.
    date accessioned2017-05-09T01:14:06Z
    date available2017-05-09T01:14:06Z
    date issued2014
    identifier issn1048-9002
    identifier othervib_136_03_031014.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156762
    description abstractThe experimental and numerical studies on farfield pyroshock responses of composite panels are presented in this paper. The purpose of this study is to find out the region of composite panel where the pyroshock response is high and thereby the panel can be used as a testing bed to examine tiny elements such as electronic parts used in spacecraft. Experiments based on biplate technology are conducted on different combination of eglass/epoxy composite panel parameters. The structural responses are analyzed using panel parameters as well as shock response spectrums (SRSs) computed from the accelerationtime histories. The experiments are carried out for a low range of chamber pressure with projectiles of varying length to get the farfield response of the test panel. The accelerations of the panel at selected locations are measured by the PCB Piezotronics (Depew, NY) accelerometers and National InstrumentsData Acquisition (NIDAQ) system (National Instruments, Austin, TX) with labview software. Finite element analysis (FEA) for the pyroshock environment is done using abaqus/Explicit software. Due to the symmetry of the structure as well as the loading, only quarter portion of the panel is analyzed. From the results, it is found that acceleration increases as thickness of composite test panel increases (about 20–70%) for all the combinations of projectile length and chamber pressure at all the points considered on the laminate. Transfer of acceleration from steel plate onto composite panel through physical connections is predominant (about 90–95% of total transfer) than that through air media between the steel plate and the composite panel. Velocity with lower momentum induces lower frequency modes to be dominant whereas velocity with higher momentum induces higher frequency modes. Normally higher accelerations (about 40–90%) are experienced at the center location than any other locations under consideration. The SRSs are obtained both from FEA and experiments. The experimental study shows good agreement with the FEA results both in acceleration time history as well as in SRS.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStudy of Far Field Pyroshock Responses of Composite Panels
    typeJournal Paper
    journal volume136
    journal issue3
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.4027223
    journal fristpage31014
    journal lastpage31014
    identifier eissn1528-8927
    treeJournal of Vibration and Acoustics:;2014:;volume( 136 ):;issue: 003
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian