4.6 Article

In-plane compression modulus and strength of Nomex honeycomb cores

期刊

JOURNAL OF SANDWICH STRUCTURES & MATERIALS
卷 24, 期 1, 页码 627-642

出版社

SAGE PUBLICATIONS LTD
DOI: 10.1177/10996362211021888

关键词

In-plane compression test; honeycomb core; compressive strength; compressive stress-strain response; collapse of honeycomb core; Nomex Paper

资金

  1. Federal Aviation Administration (FAA) [16-G-006]
  2. National Institute of Aerospace (NIA)

向作者/读者索取更多资源

The experimental study examined the stress-strain response and deformation mechanism of Nomex honeycomb cores under in-plane compression, revealing that cores with thin walls exhibit bending deformation and failure, while cores with thicker walls fail due to shear-type instability of cells. Increasing core density results in decreased failure strain. Comparison with micromechanical predictions showed variations in normalized modulus and strength values among different cores. The study also extracted the modulus and bending strength of Nomex paper based on average modulus and strength results, which were in reasonable agreement with previous tensile test results and composite micromechanics.
The stress-strain response and deformation mechanism of a range of Nomex honeycomb cores tested under in-plane compression has been examined experimentally. The cores with a thin wall displayed extensive bending deformation of the cell walls inclined to the horizontal (loading is vertical) and failed in bending. The cores with thicker walls failed by a shear-type instability of the cells indicated by tilting of vertical cell wall segments. The failure strain decreased with increasing core density. The modulus and compressive strength of the core were compared to micromechanical predictions. Normalized modulus and strength values varied between the various cores. The average modulus and strength results allow backing out of the modulus and bending strength of the Nomex paper. The results were in reasonable agreement with published tensile test results and composite micromechanics.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.6
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据