YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Manufacturing Science and Engineering
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Manufacturing Science and Engineering
    • 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

    Thermal Stresses in Spherical Case-Bonded Propellant Grains

    Source: Journal of Manufacturing Science and Engineering:;1962:;volume( 084 ):;issue: 001::page 144
    Author:
    Irvin Krause
    ,
    Bernard W. Shaffer
    DOI: 10.1115/1.3667394
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Expressions are derived for the bond stresses induced by a radially symmetric temperature distribution in spherical propellant grains bonded to spherical casings. Equations for the evaluation of radial and tangential stresses in the propellant and its casing have also been derived. Both solid and hollow propellant grains have been investigated. Design considerations have been developed to enable the designer to minimize the bond stress. A comparison between the hollow and solid spherical propellant assembly shows that the hollow sphere has a lower bond stress than the solid sphere, assuming all other factors are the same.
    keyword(s): Thermal stresses , Propellants , Stress , Manufacturing , Design , Equations AND Temperature distribution ,
    • Download: (1.817Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Thermal Stresses in Spherical Case-Bonded Propellant Grains

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/92068
    Collections
    • Journal of Manufacturing Science and Engineering

    Show full item record

    contributor authorIrvin Krause
    contributor authorBernard W. Shaffer
    date accessioned2017-05-08T23:06:36Z
    date available2017-05-08T23:06:36Z
    date copyrightFebruary, 1962
    date issued1962
    identifier issn1087-1357
    identifier otherJMSEFK-27458#144_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/92068
    description abstractExpressions are derived for the bond stresses induced by a radially symmetric temperature distribution in spherical propellant grains bonded to spherical casings. Equations for the evaluation of radial and tangential stresses in the propellant and its casing have also been derived. Both solid and hollow propellant grains have been investigated. Design considerations have been developed to enable the designer to minimize the bond stress. A comparison between the hollow and solid spherical propellant assembly shows that the hollow sphere has a lower bond stress than the solid sphere, assuming all other factors are the same.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermal Stresses in Spherical Case-Bonded Propellant Grains
    typeJournal Paper
    journal volume84
    journal issue1
    journal titleJournal of Manufacturing Science and Engineering
    identifier doi10.1115/1.3667394
    journal fristpage144
    journal lastpage148
    identifier eissn1528-8935
    keywordsThermal stresses
    keywordsPropellants
    keywordsStress
    keywordsManufacturing
    keywordsDesign
    keywordsEquations AND Temperature distribution
    treeJournal of Manufacturing Science and Engineering:;1962:;volume( 084 ):;issue: 001
    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