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MATERIALS-BY-DESIGN METHODOLOGY APPLIED TO POLYMER COMPOSITES FOR ENHANCED BALLISTIC PENETRATION RESISTANCE

机译:应用于聚合物复合材料的逐个设计方法,用于增强弹道渗透性

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Polymeric-fiber-reinforced, polymer-matrix armor-grade composite materials with a superior ballistic limit are traditionally developed using legacy knowledge and trial-and-error empiricism. This approach is generally quite costly and time-consuming and, hence, new (faster and more economical) approaches are needed for the development of new and improved armor-grade composite materials. One of these new approaches utilizes the so-called materials-by-design methodology. Within this methodology, extensive use is made of the computer-aided engineering (CAE) analyses and of the empirically-/theoretically-established functional relationships between: (a) the performance of the armor-grade-composite-protected structure and the properties of the composite material of which the structure is made; (b) composite-material properties and material microstructure (as characterized at different length-scales); and (c) material microstructure and material synthesis/processing route(s). In the present work, a preliminary effort is made towards applying the materials-by-design methodology to the development of armor-grade composite materials and protective structures with superior ballistic-penetration resistance. Specifically, CAE analyses are utilized to establish functional relationships between the attributes/properties of the composite material and the ballistic- penetration-resistance of the associated protective structure, and to identify the combination of these properties which maximizes the penetration resistance. Once the optimal set of material- model parameters is established, the microstructural features the material must possess to acquire this set of material-model parameters are identified. Finally, the material synthesis/processing route(s) required to achieve the desired set of material microstructural features is established.
机译:具有优异的弹道极限的聚合物 - 纤维增强的聚合物 - 基质铠装级复合材料,传统上使用遗留知识和试验和错误经验主义开发出具有优异的弹道限制。这种方法通常是完全昂贵且耗时的,因此,需要新的(更快,更经济)的方法来开发新的和改进的装甲级复合材料。这些新方法之一利用所谓的逐个设计方法。在该方法中,广泛的用途是由计算机辅助工程(CAE)分析以及经验 - /理论上建立的功能关系:(a)铠装 - 级复合保护结构和性质的性能制造结构的复合材料; (b)复合材料性质和材料微观结构(如在不同的长度尺度上表征); (c)材料微观结构和材料合成/加工途径。在目前的工作中,初步努力旨在将材料级化学方法应用于铠装级复合材料和具有优异的弹道渗透性的保护结构。具体地,CAE分析用于建立复合材料的属性/性能与相关保护结构的弹道渗透性之间的功能关系,并鉴定这些性能最大化渗透性的组合。一旦建立了最佳的材料型号参数,就识别了材料的微观结构特征必须具有获取该组材料模型参数。最后,建立了达到所需材料组织微观结构特征所需的材料合成/加工途径。

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