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    Single-Angle Compression Members with Both Legs Bolted at the Ends: Design Implications from an Experimental Study

    Source: Journal of Structural Engineering:;2018:;Volume ( 144 ):;issue: 009
    Author:
    Tian Li;Guo Liulu;Qu Bing
    DOI: 10.1061/(ASCE)ST.1943-541X.0002158
    Publisher: American Society of Civil Engineers
    Abstract: Single-angle compression members are widely used in civil structures. However, determination of the compressive strength of a single-angle compression member based on the classic stability theory and with an explicit consideration of the loading eccentricity is onerous, lengthy, and impractical for design. Although the approximate effective slenderness ratios recommended in current standards help simplify the design process, these recommendations do not cover single-angle compression members with both legs bolted at the ends (which can be a design alternative to angle members with other end conditions). Focusing on angle members with equal legs, we tested 47 specimens to generate a result database for the compressive strengths of single-angle compression members with both legs bolted at the ends. The test results suggest that existing design provisions, together with the effective length factors associated with the ideal end conditions, may not be the best options for design of single-angle compression members with both legs bolted at the ends. Based on the test results, an empirical model was developed to determine the effective slenderness ratios of single-angle members with both legs bolted at the ends. The model is compatible with existing design documents. Analysis results show that the proposed model provides reasonable predictions and can be used for future design.
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      Single-Angle Compression Members with Both Legs Bolted at the Ends: Design Implications from an Experimental Study

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4249481
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    contributor authorTian Li;Guo Liulu;Qu Bing
    date accessioned2019-02-26T07:48:01Z
    date available2019-02-26T07:48:01Z
    date issued2018
    identifier other%28ASCE%29ST.1943-541X.0002158.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4249481
    description abstractSingle-angle compression members are widely used in civil structures. However, determination of the compressive strength of a single-angle compression member based on the classic stability theory and with an explicit consideration of the loading eccentricity is onerous, lengthy, and impractical for design. Although the approximate effective slenderness ratios recommended in current standards help simplify the design process, these recommendations do not cover single-angle compression members with both legs bolted at the ends (which can be a design alternative to angle members with other end conditions). Focusing on angle members with equal legs, we tested 47 specimens to generate a result database for the compressive strengths of single-angle compression members with both legs bolted at the ends. The test results suggest that existing design provisions, together with the effective length factors associated with the ideal end conditions, may not be the best options for design of single-angle compression members with both legs bolted at the ends. Based on the test results, an empirical model was developed to determine the effective slenderness ratios of single-angle members with both legs bolted at the ends. The model is compatible with existing design documents. Analysis results show that the proposed model provides reasonable predictions and can be used for future design.
    publisherAmerican Society of Civil Engineers
    titleSingle-Angle Compression Members with Both Legs Bolted at the Ends: Design Implications from an Experimental Study
    typeJournal Paper
    journal volume144
    journal issue9
    journal titleJournal of Structural Engineering
    identifier doi10.1061/(ASCE)ST.1943-541X.0002158
    page6018004
    treeJournal of Structural Engineering:;2018:;Volume ( 144 ):;issue: 009
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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