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Optimum first failure load design of one/two-core sandwich plates under blast loads, and their ultimate loads

机译:爆炸载荷下单芯/两芯夹芯板的最佳首次破坏载荷设计及其极限载荷

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We consider a sandwich plate with face sheets made of unidirectional fiber-reinforced composite with fibers being either glass, or carbon or aramid and the core made of balsa wood loaded by a blast pressure, and find optimal geometries and materials for maximizing the first failure load. While analyzing the problem, we assume that the areal density is fixed and use the Nest-Site Selection optimization algorithm, a third-order shear and normal deformable plate theory, a one-step stress recovery scheme, and the Tsai-Wu failure criterion. We also delineate the effect on the first failure load of inertia forces and uncertainties in values of various parameters. For a sandwich plate optimally designed for the first failure load, we find the ultimate load by progressively degrading elasticities of failed elements. We find that the optimal single-core sandwich designs are symmetric about the mid-surface with thick face sheets and the optimal two-core sandwich designs have a thin middle face sheet, and thick top and bottom face sheets. The first failure load of the optimal clamped single-core (two-core) design is approximately 20% (30%) more than that of the corresponding simply-supported plate. For simply-supported (clamped) sandwich structures, the failure initiates at the centroid (center of the clamped edge) of either the top or the bottom surfaces. It is also found that the first failure occurs in a face sheet (core) due to the in-plane transverse axial stress (transverse shear stress) exceeding its critical value. The collapse load of a clamped (simply-supported) sandwich structure is approximately 15%-30% (0%-17%) higher than the first failure load. The maximum deflection of the collapsed structure may be in a direction opposite to that of the applied load. A novelty of the work is in considering inertia effects in ascertaining the first and the ultimate failure loads and quantifying the benefits, if any, of two-core over one-core sandwich structures, and determining effects of uncertainties in values of parameters.
机译:我们考虑一种夹芯板,其面板由单向纤维增强复合材料制成,其中纤维为玻璃,碳或芳族聚酰胺,芯层由轻木材料承受爆炸压力,并找到最佳的几何形状和材料,以最大程度地提高首次破坏载荷。在分析问题时,我们假设面密度是固定的,并使用Nest-Site选择优化算法,三阶剪切和法向可变形板理论,一步式应力恢复方案以及Tsai-Wu破坏准则。我们还描述了惯性力对第一失效载荷的影响以及各种参数值的不确定性。对于最适合首次破坏载荷的夹层板,我们通过逐渐降低破坏单元的弹性来找到极限载荷。我们发现,最佳的单芯夹心设计是围绕着厚表面的中表面对称的,而最佳的两芯夹心设计是具有薄的中间面板和厚的顶面和底面。最佳夹紧单芯(两芯)设计的第一个失效载荷比相应的简单支撑板高约20%(30%)。对于简单支撑(夹紧的)夹层结构,破坏始于顶面或底面的质心(夹紧边缘的中心)。还发现,由于面内横向轴向应力(横向剪切应力)超过其临界值,第一失效发生在面板(芯)中。夹紧(简单支撑)夹层结构的坍塌载荷比第一破坏载荷大约高15%-30%(0%-17%)。塌陷结构的最大挠度可以在与所施加的载荷相反的方向上。这项工作的新颖性在于在确定惯性效应时确定第一和最终破坏载荷,并量化两芯与一芯夹心结构之间的收益(如果有),以及确定参数值不确定性的影响。

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