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Assessment of Intralaminar Progressive Damage and Failure Analysis Methods Using an Efficient Evaluation Framework

机译:使用有效的评估框架评估腹腔内进行性损伤和衰竭分析方法

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Reducing the timeline for development and certification for composite structureshas been a long standing objective of the aerospace industry. This timeline can befurther exacerbated when attempting to integrate new fiber-reinforced compositematerials due to the large number of testing required at every level of design.Computational progressive damage and failure analysis (PDFA) attempts to mitigatethis effect; however, new PDFA methods have been slow to be adopted in industrysince material model evaluation techniques have not been fully defined. This studypresents an efficient evaluation framework which uses a piecewise verification andvalidation (V&V) approach for PDFA methods. Specifically, the framework isapplied to evaluate PDFA research codes within the context of intralaminar damage.Methods are incrementally taken through various V&V exercises specifically tailoredto study PDFA intralaminar damage modeling capability. Finally, methods areevaluated against a defined set of success criteria to highlight successes andlimitations.
机译:减少复合结构开发和认证的时间表 一直是航空航天业的长期目标。该时间表可以是 尝试整合新的纤维增强复合材料时,情况进一步恶化 由于在每个设计水平上都需要进行大量测试,因此这些材料是必需的。 计算渐进式破坏和失效分析(PDFA)试图减轻 这种效果;但是,新的PDFA方法在行业中的采用速度缓慢 由于尚未完全定义材料模型评估技术。这项研究 提出了一个有效的评估框架,该框架使用了分段验证和 PDFA方法的验证(V&V)方法。具体来说,框架是 用于评估层内损伤范围内的PDFA研究规范。 通过专门定制的各种V&V练习逐步采用方法 研究PDFA层内损伤建模能力。最后,方法是 根据定义的一组成功标准进行评估,以突出成功和 局限性。

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