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    Uniformly Stiffened Cantilever Plates under Bending

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 003::page 04025009-1
    Author:
    Kaushal Kumar
    ,
    Gyani Jail Singh
    ,
    Ishu Sharma
    ,
    Krishna Pratap Singh
    ,
    Rajesh Kumar
    DOI: 10.1061/JAEEEZ.ASENG-5495
    Publisher: American Society of Civil Engineers
    Abstract: A number of studies have shown that T-beams exhibit positive shear lag under bending; however, a detailed stress distribution profile of uniformly stiffened plates is rarely presented. The present study analyzes uniformly stiffened plates under bending. The stiffened plate model is discretized using an energy-based variational approach. In order to develop differential equations, the principle of minimum potential energy is applied. Based on simplified assumptions, simple, closed-form solutions are obtained for normal stress distributions. Unlike what has been reported for T-beams, stiffeners applied uniformly across the width of a plate change the direction of shear flow and thereby alter the normal stress distribution profile. It remains true that the peak stress of a cantilever stiffened plate remains on the centerline of the plate as that of a T-beam, but the stress distribution profile demonstrates a negative shear lag effect in this case. For a given aspect ratio (w/l) and a constant E/G ratio, the stress concentration is strongly influenced by the shear flow capacity of the stiffened plates contrary to T-beams where the stress concentration is determined by the relative stiffness of the flange. A high E/G ratio results in a higher stress concentration on the stiffened plate. In the case of an infinitely wide cantilever stiffened plate, peak stress factors converge to two. In the case of uniform and point loading, stiffened plates with a width four times the length (w/l=2) have a stress concentration approximately 8.57% and 11.31% lower than infinitely wide beams. In the case of w/l=4, this error is negligible. When the w/l ratio increases, the negative shear lag intensity increases, and the positive shear lag region decreases. The present research results have been verified by finite-element analysis (FEA) and are in close agreement with those reported in the literature.
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      Uniformly Stiffened Cantilever Plates under Bending

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    contributor authorKaushal Kumar
    contributor authorGyani Jail Singh
    contributor authorIshu Sharma
    contributor authorKrishna Pratap Singh
    contributor authorRajesh Kumar
    date accessioned2025-08-17T22:29:51Z
    date available2025-08-17T22:29:51Z
    date copyright5/1/2025 12:00:00 AM
    date issued2025
    identifier otherJAEEEZ.ASENG-5495.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307016
    description abstractA number of studies have shown that T-beams exhibit positive shear lag under bending; however, a detailed stress distribution profile of uniformly stiffened plates is rarely presented. The present study analyzes uniformly stiffened plates under bending. The stiffened plate model is discretized using an energy-based variational approach. In order to develop differential equations, the principle of minimum potential energy is applied. Based on simplified assumptions, simple, closed-form solutions are obtained for normal stress distributions. Unlike what has been reported for T-beams, stiffeners applied uniformly across the width of a plate change the direction of shear flow and thereby alter the normal stress distribution profile. It remains true that the peak stress of a cantilever stiffened plate remains on the centerline of the plate as that of a T-beam, but the stress distribution profile demonstrates a negative shear lag effect in this case. For a given aspect ratio (w/l) and a constant E/G ratio, the stress concentration is strongly influenced by the shear flow capacity of the stiffened plates contrary to T-beams where the stress concentration is determined by the relative stiffness of the flange. A high E/G ratio results in a higher stress concentration on the stiffened plate. In the case of an infinitely wide cantilever stiffened plate, peak stress factors converge to two. In the case of uniform and point loading, stiffened plates with a width four times the length (w/l=2) have a stress concentration approximately 8.57% and 11.31% lower than infinitely wide beams. In the case of w/l=4, this error is negligible. When the w/l ratio increases, the negative shear lag intensity increases, and the positive shear lag region decreases. The present research results have been verified by finite-element analysis (FEA) and are in close agreement with those reported in the literature.
    publisherAmerican Society of Civil Engineers
    titleUniformly Stiffened Cantilever Plates under Bending
    typeJournal Article
    journal volume38
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5495
    journal fristpage04025009-1
    journal lastpage04025009-12
    page12
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 003
    contenttypeFulltext
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