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Effects of Plate Slenderness on the Ultimate Strength Behaviour of Foam Supported Steel Plate Elements

机译:平板细长度对泡沫支撑钢板单元极限强度行为的影响

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摘要

Plate elements in fully profiled sandwich panels are generally subjected to local buckling failure modes and this behaviour is treated in design by using the conventional effective width method for plates with a width to thickness (b/t) ratio less than 100. If the plate elements are very slender (b/t>1000), the panel failure is governed by wrinkling instead of local buckling and the strength is determined by the flexural wrinkling formula. The plate elements in fully profiled sandwich panels do not fail by wrinkling as their b/t ratio is generally in the range of 100 to 600. For this plate slenderness region, it was found that the current effective width formula overestimates the strength of the fully profiled sandwich panels whereas the wrinkling formula underestimates it. Hence a new effective width design equation has been developed for practical plate slenderness values. However, no guidelines exist to identify the plate slenderness (b/t) limits defining the local buckling, wrinkling and the intermediate regions so that appropriate design rules can be used based on plate slenderness ratios. A research study was therefore conducted using experimental and numerical studies to investigate the effect of plate slenderness ratio on the ultimate strength behaviour of foam supported steel plate elements. This paper presents the details of the study and the results.
机译:完全成型的夹心板中的板元件通常会遭受局部屈曲破坏模式,这种行为在设计中通过使用常规的有效宽度方法对宽厚比(b / t)小于100的板进行处理。它们非常纤细(b / t> 1000),面板破坏由起皱而不是局部屈曲控制,强度由弯曲起皱公式决定。完全成型的夹心板中的板元件不会因皱纹而失效,因为它们的b / t比通常在100到600的范围内。对于该板细长区域,我们发现当前的有效宽度公式高估了整个板的强度。异形夹芯板,而起皱的公式则低估了它。因此,已经针对实际的板细长度值开发了新的有效宽度设计方程。但是,目前尚无准则来确定定义局部屈曲,起皱和中间区域的板的伸长率(b / t)限值,因此可以根据板的伸长率使用适当的设计规则。因此,使用实验和数值研究进行了研究,以研究板的长宽比对泡沫支撑钢板元件的极限强度行为的影响。本文介绍了研究的细节和结果。

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