首页> 外文学位 >Ultimate compression after impact load prediction in graphite/epoxy coupons using neural network and multivariate statistical analyses.
【24h】

Ultimate compression after impact load prediction in graphite/epoxy coupons using neural network and multivariate statistical analyses.

机译:使用神经网络和多元统计分析预测石墨/环氧树脂试样中的冲击载荷后的最终压缩。

获取原文
获取原文并翻译 | 示例

摘要

The goal of this research was to accurately predict the ultimate compressive load of impact damaged graphite/epoxy coupons using a Kohonen self-organizing map (SOM) neural network and multivariate statistical regression analysis (MSRA). An optimized use of these data treatment tools allowed the generation of a simple, physically understandable equation that predicts the ultimate failure load of an impacted damaged coupon based uniquely on the acoustic emissions it emits at low proof loads. Acoustic emission (AE) data were collected using two 150 kHz resonant transducers which detected and recorded the AE activity given off during compression to failure of thirty-four impacted 24-ply bidirectional woven cloth laminate graphite/epoxy coupons. The AE quantification parameters duration, energy and amplitude for each AE hit were input to the Kohonen self-organizing map (SOM) neural network to accurately classify the material failure mechanisms present in the low proof load data. The number of failure mechanisms from the first 30% of the loading for twenty-four coupons were used to generate a linear prediction equation which yielded a worst case ultimate load prediction error of 16.17%, just outside of the +/-15% B-basis allowables, which was the goal for this research. Particular emphasis was placed upon the noise removal process which was largely responsible for the accuracy of the results.
机译:这项研究的目的是使用Kohonen自组织图(SOM)神经网络和多元统计回归分析(MSRA)准确预测冲击损坏的石墨/环氧树脂试样的最终压缩载荷。这些数据处理工具的优化使用允许生成一个简单的,物理上易于理解的方程式,该方程式可以唯一地基于低验证载荷下发出的声发射来预测受影响的损坏试样的最终破坏载荷。使用两个150 kHz共振换能器收集声发射(AE)数据,该换能器检测并记录了在压缩过程中由于破坏了34个受影响的24层双向机织织物层压石墨/环氧树脂试样而散发的AE活性。将每个AE命中的AE量化参数持续时间,能量和幅度输入到Kohonen自组织图(SOM)神经网络,以准确地分类低证明载荷数据中存在的材料破坏机制。从二十四个试样的载荷的前30%开始的故障机理数量用于生成线性预测方程,该方程产生的最坏情况下,最终载荷预测误差为16.17%,刚好在+/- 15%B-之外。基础允许量,这是本研究的目标。特别强调了噪声消除过程,这在很大程度上决定了结果的准确性。

著录项

  • 作者

    Gregoire, Alexandre David.;

  • 作者单位

    Embry-Riddle Aeronautical University.;

  • 授予单位 Embry-Riddle Aeronautical University.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.A.E.
  • 年度 2011
  • 页码 229 p.
  • 总页数 229
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号