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首页> 外文期刊>International journal of impact engineering >Development Of Reliable Modeling Methodologies For Fan Blade Out Containment Analysis - Part I: Experimental Studies
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Development Of Reliable Modeling Methodologies For Fan Blade Out Containment Analysis - Part I: Experimental Studies

机译:风机叶片熄火分析可靠模型方法的开发-第一部分:实验研究

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摘要

High strength woven fabrics are ideal candidate materials for use in structural systems where high energy absorption is required. One of the more widely used applications for woven fabrics is in propulsion engine containment systems. In this first part of a two-part paper, details of the experiments to characterize the behavior of dry fabrics including Kevlar~R and Zylon~R are presented. The experimental program to characterize the behavior of 1420 Denier Kevlar~R 49 17 × 17, 500 Denier Zylon~R AS 35 × 35, and 1500 Denier Zylon~R 17 × 17 are discussed. The primary objective is to use the experimental results in the development of a constitutive model that can be used in an explicit finite element analysis program. These include Tension Tests in both the warp and fill directions of the fabric, Trellising Shear Tests and Friction Tests between fabric layers. The results from these tests provide the basis for development of the constitutive model - relating stresses to strains, characterizing failure and interaction between fabric layers. In addition to these basic material tests, tests on systems built with fabric wraps were also conducted. Ballistic tests of containment wraps subjected to a high velocity projectile were carried out at NASA-Glenn Research Center. While these tests provide a comparison between the energy absorbing characteristics of the three fabrics, they also provide benchmark results to validate the developed finite element methodology discussed in the second part of this paper.
机译:高强度机织织物是用于需要高能量吸收的结构系统的理想候选材料。机织物的更广泛使用的应用之一是在推进发动机密封系统中。在由两部分组成的论文的第一部分中,详细介绍了表征干织物(包括Kevlar〜R和Zylon〜R)行为的实验细节。讨论了表征1420 Denier Kevlar〜R 49 17×17、500 Denier Zylon〜R AS 35×35和1500 Denier Zylon〜R 17×17行为的实验程序。主要目的是将实验结果用于本构模型的开发,该模型可用于显式有限元分析程序。这些包括在织物的经向和填充方向上的拉伸测试,在织物层之间的网格剪切测试和摩擦测试。这些测试的结果为建立本构模型提供了基础-将应力与应变相关联,表征了织物层之间的破坏和相互作用。除了这些基本的材料测试之外,还对使用织物包裹物构建的系统进行了测试。在美国国家航空航天局格伦研究中心进行了高速弹丸对安全壳包裹物的弹道测试。虽然这些测试提供了三种织物的能量吸收特性之间的比较,但它们还提供了基准结果,以验证本文第二部分中讨论的已开发的有限元方法。

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