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INVESTIGATION OF CONSTRAINT EFFECTS ON FLAW GROWTH IN COMPOSITE LAMINATES.

机译:复合层板中反跳生长的约束效应研究。

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摘要

An investigation was conducted to study the constraint effects on flaw growth in composite laminates. Results were presented for the case of a transverse flaw in an interior ply perpendicular to the loading axis. Two orientations of the flawed ply were examined (0 and 90 degrees), and two distinctly different constraint situations were studied (cross-ply constraint and biaxial constraint).; Throughout the study, various nondestructive testing methods were employed to evaluate the material response and to determine the damage and damage growth in the specimens. These techniques include replication, ultrasonic c-scan, ultrasonic attenuation, acoustic emission, x-radiography, thermography and stiffness measurement.; The effects of constraint on the response of composite materials can be classified in two categories: (a) in-plane effects and (b) through-the-thickness effects. In-plane constraint is the principal contributor to notched strength and changes in notched strength under quasi-static loading. Through-the-thickness constraint controls the pattern and spacing of transverse cracks in the off-axis plies to form a characteristic damage state in the laminates. Out-of-plane stresses produced by constraints are influential on the growth of damage along ply interfaces, especially during cyclic loading.; The mode of damage and the extent of damage in constrained notched plies are governed by the stress state in those plies, as determined by the constraining plies, and the relationship of the stress state to the strength state. Maximum constraint on the flawed ply does not produce minimum damage in the laminate; and the lesser degree of damage (in terms of axial splitting and delamination) does not necessarily result in a higher laminate strength or long fatigue lifes. In the design of composite structures, a compromise has to be reached with regard to optimizing material parameters such as strength, stiffness, fatigue life and residual strength. In maximizing one parameter, one might have to sacrifice other requirements on the other material properties in the design.
机译:进行了一项研究,以研究复合材料层压板中缺陷生长的约束效应。给出了在垂直于加载轴的内部层中出现横向裂纹的结果。检查了缺陷层的两个方向(0度和90度),并研究了两种截然不同的约束情况(跨层约束和双轴约束)。在整个研究过程中,采用了各种无损检测方法来评估材料的响应并确定样品的损伤和损伤的增长。这些技术包括复制,超声c扫描,超声衰减,声发射,X射线照相,热成像和硬度测量。约束对复合材料响应的影响可分为两类:(a)面内效应和(b)厚度方向效应。平面约束是准静态载荷下缺口强度和缺口强度变化的主要因素。厚度限制控制离轴帘布层中横向裂纹的图案和间距,以在层压板中形成特征性的损坏状态。约束产生的平面外应力对沿层界面的损伤的增长有影响,特别是在循环载荷期间。受约束的缺口板的损坏方式和破坏程度取决于约束板确定的应力状态以及应力状态与强度状态之间的关系。对有缺陷的层的最大限制不会在层压板中产生最小的损坏;较小程度的损坏(就轴向裂开和分层而言)并不一定会导致层压板强度更高或疲劳寿命更长。在复合结构的设计中,必须在优化材料参数(例如强度,刚度,疲劳寿命和残余强度)方面做出折衷。在最大化一个参数时,可能不得不牺牲设计中其他材料特性的其他要求。

著录项

  • 作者

    YEUNG, PETER CHUN-NGOK.;

  • 作者单位

    Virginia Polytechnic Institute and State University.;

  • 授予单位 Virginia Polytechnic Institute and State University.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 1979
  • 页码 107 p.
  • 总页数 107
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;
  • 关键词

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