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Tailoring thermal residual stresses to maximize buckling loads in composite plates.

机译:调整热残余应力以最大程度地提高复合板的屈曲载荷。

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摘要

The effect of tailoring the thermal stresses in composite plates is studied. Traditionally thermal stresses have been seen as a problem that must be minimized to prevent premature failure. While this is a concern, thermal residual stresses can also be used to prestress a composite plate so that the plate resists buckling loads. Numerous numerical studies were performed to determine the effect of various parameters such as the temperature change the plate undergoes, the aspect ratio, boundary conditions and the size and location of stiffeners. Then plates under various loading configurations were optimized to determine the configuration that results in the largest increase in buckling load, and how much improvement is possible for each configuration. The optimized plates were then analyzed neglecting the effects of temperature and it was found that thermal residual stresses had a large effect on the modeled plate's buckling load.
机译:研究了调整复合板中热应力的效果。传统上,热应力已被视为一个问题,必须将其最小化以防止过早失效。尽管这是一个值得关注的问题,但也可以使用热残余应力对复合板进行预应力,以使该板抵抗屈曲载荷。进行了许多数值研究,以确定各种参数的影响,例如板的温度变化,纵横比,边界条件以及加劲肋的尺寸和位置。然后,对各种加载配置下的板进行优化,以确定导致屈曲负载最大增加的配置,以及每种配置可以进行多少改进。然后在忽略温度影响的情况下对优化的板进行了分析,发现热残余应力对模型板的屈曲载荷有很大的影响。

著录项

  • 作者

    Rose, Tonya Leigh.;

  • 作者单位

    University of Toronto (Canada).;

  • 授予单位 University of Toronto (Canada).;
  • 学科 Engineering Aerospace.
  • 学位 M.A.Sc.
  • 年度 2000
  • 页码 74 p.
  • 总页数 74
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:47:34

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