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    Effect of Localized Bending at Through‐Flaws in Pressurized Composite Cylinders

    Source: Journal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 004
    Author:
    Kevin J. Saeger
    ,
    Paul A. Lagace
    DOI: 10.1061/(ASCE)0893-1321(1993)6:4(381)
    Publisher: American Society of Civil Engineers
    Abstract: An analytical and experimental investigation was conducted to determine the effect of localized bending at through‐flaws in pressurized composite cylinders. A finite‐difference solution was formulated to determine the stress, strain, and displacement fields in the vicinity of a slit. Tests were conducted on 305‐mm‐diameter cylinders made from graphite/epoxy fabric in a
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      Effect of Localized Bending at Through‐Flaws in Pressurized Composite Cylinders

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/79536
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    contributor authorKevin J. Saeger
    contributor authorPaul A. Lagace
    date accessioned2017-05-08T22:23:41Z
    date available2017-05-08T22:23:41Z
    date copyrightOctober 1993
    date issued1993
    identifier other43930495.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/79536
    description abstractAn analytical and experimental investigation was conducted to determine the effect of localized bending at through‐flaws in pressurized composite cylinders. A finite‐difference solution was formulated to determine the stress, strain, and displacement fields in the vicinity of a slit. Tests were conducted on 305‐mm‐diameter cylinders made from graphite/epoxy fabric in a
    publisherAmerican Society of Civil Engineers
    titleEffect of Localized Bending at Through‐Flaws in Pressurized Composite Cylinders
    typeJournal Paper
    journal volume6
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1993)6:4(381)
    treeJournal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 004
    contenttypeFulltext
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