首页> 外文期刊>Thin-Walled Structures >Effect of moment of inertia on elastic stability of rectangular webs for thin-walled beams under a transverse load
【24h】

Effect of moment of inertia on elastic stability of rectangular webs for thin-walled beams under a transverse load

机译:惯性矩对横向荷载作用下薄壁矩形矩形腹板弹性稳定性的影响

获取原文
获取原文并翻译 | 示例
           

摘要

So far, the equations for buckling capacity of web panels focus on thin-walled beams with very strong flanges. In this paper, elastic buckling behavior of web panels of thin-walled beams with weak flanges is further studied, aiming at a buckling coefficient formula unifying the effect of both weak and strong flanges. A new parameter, the flange-to-web ratio of moment of inertia, is proposed to characterize the effect of flanges. Then, a semi-analytical method is applied to investigate the buckling behavior of simply supported web panels, in two cases, inclusive or exclusive of effect of the moment of inertia of flanges. It is revealed that elastic buckling load, in particular, the buckling coefficient of web panel is a function of two key parameters, web aspect ratio and flange-to-web ratio of moment of inertia. Meanwhile, a finite element analysis (FEA) model allowing for the sensitivity of boundary conditions is validated by comparing with the semi-analytical solution to the case exclusive of effect of the moments of inertia of flanges. Next, numerical results are utilized to illustrate the influence of the previous parameters, which verify the increase of buckling coefficient with flange-to-web ratio of moment of inertia or the decrease of buckling coefficient with web aspect ratio. Besides, it also verifies that for the same flange-to-web ratio of moment of inertia, the buckling behavior of square web panels is closer to the uniform shear buckling than other rectangular web panels. Finally, an accurate design formula is proposed to calculate buckling coefficient of web panel.
机译:到目前为止,腹板的屈曲能力方程主要集中在具有很强凸缘的薄壁梁上。本文针对弱翼缘薄壁梁腹板的弹性屈曲行为,以统一弱,强翼缘作用的屈曲系数公式为研究对象。提出了一个新参数,即法兰与腹板的惯性矩比,以表征法兰的作用。然后,在两种情况下(包括或不包括法兰惯性矩的影响),采用半分析方法来研究简单支撑腹板的屈曲行为。结果表明,弹性屈曲载荷,特别是腹板的屈曲系数是两个关键参数的函数,腹板的长宽比和法兰与腹板的惯性矩之比。同时,通过与半解析解进行比较,在不考虑法兰惯性矩影响的情况下,验证了允许边界条件敏感的有限元分析(FEA)模型。接下来,利用数值结果说明了先前参数的影响,这些参数验证了屈曲系数随翼缘-腹板惯性比的增加而增加,或随腹板纵横比的降低而降低。此外,它还验证了对于相同的法兰与腹板惯性比,方形腹板的屈曲行为比其他矩形腹板更接近均匀的剪切屈曲。最后,提出了一种精确的设计公式来计算腹板的屈曲系数。

著录项

  • 来源
    《Thin-Walled Structures》 |2014年第12期|34-41|共8页
  • 作者单位

    Department of Astronautic Science and Mechanics, Harbin Institute of Technology, Harbin 150001, China;

    Department of Astronautic Science and Mechanics, Harbin Institute of Technology, Harbin 150001, China;

    Department of Astronautic Science and Mechanics, Harbin Institute of Technology, Harbin 150001, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Elastic buckling; Web panel; Transverse loading; Moment of inertia; Design formula;

    机译:弹性屈曲网络面板;横向载荷;转动惯量;设计公式;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号