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Post-buckling behaviour and strength of multi-stiffened aluminium panels under combined axial compression and lateral pressure

机译:复合加筋铝板在轴向压缩和侧向压力作用下的后屈曲特性和强度

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This paper presents the results of complementary numerical study done in the continuation of the activities carried out by the Committee IIl.1 "Ultimate Strength" of ISSC2003 (Ref. [28] ).The main focus of the paper concerns the post-buckling behaviour and strength characteristics of the aluminium multi-stiffened panels under combined axial compression and lateral pressure. The finite element model proposed by the Committee IIl.l "Ultimate Strength" of 1SSC2003 is used in the present investigation. Material is aluminium alloy AA6082-T6 and the multi-stiffened panel is a triple-span structure. Stiffeners are of either extruded or non-extruded angle-bar profiles. An initial deflection is imposed on the model in a procedure similar to that applied by the Committee IIl.1. General purpose finite element code ANSYS is used for non-linear elastic-plastic analyses. Main objectives are to study the influence of initial deflections and also HAZ on the post-buckling behaviour and collapse characteristics of aluminium stiffened panels under combined axial compression and lateral pressure. Different values of lateral pressure are exerted on the model in a systematic manner to simulate various levels of lateral pressure loading on multi-stiffened aluminium panels used in the construction of high-speed crafts.
机译:本文介绍了继续进行的ISSC2003 IIl.1“极限强度”委员会活动的补充数值研究的结果(参考文献[28])。本文的主要重点在于屈曲后的行为。轴向压缩和侧向压力作用下铝加劲板的强度和强度特性。 1SSC2003的委员会II.1“极限强度”提出的有限元模型用于本研究。材料为铝合金AA6082-T6,多层板为三跨结构。加劲肋可以是挤压型材也可以是非挤压型材。对模型的初始挠曲采用与委员会II.1相似的程序。通用有限元代码ANSYS用于非线性弹塑性分析。主要目的是研究在轴向压缩和侧向压力作用下,初始挠度以及热影响区对铝加劲板的屈曲后行为和坍塌特性的影响。以系统的方式将不同的侧向压力值施加到模型上,以模拟高速船制造中使用的多加劲铝板上各种水平的侧向压力载荷。

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