Development and Verification of an Analytic Technique to Determine the Stiffness Parameters of Braided Tubular Parts

S. A. Samipur; Ya. S. Danilov

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Development and Verification of an Analytic Technique to Determine the Stiffness Parameters of Braided Tubular Parts

机译：开发和验证一种用于确定编织管状零件刚度参数的分析技术

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摘要

This paper deals with development and verification of an analytical technique for determining the stiffness parameters of composite tubular aerospace structures manufactured by radial braiding and transfer molding.

机译：本文介绍了一种分析技术的开发和验证，该技术用于确定径向编织和传递模塑制造的复合材料管状航空航天结构的刚度参数。

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来源
《Russian Aeronautics》 |2016年第4期|460-465|共6页
作者
S. A. Samipur; Ya. S. Danilov;
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作者单位

Tupolev Kazan National Research Technical University;

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原文格式 PDF
正文语种英语
中图分类航空;
关键词
Braided composite; Bi- and triaxial braiding; Mathematical model; Mechanical properties; Computer simulation;

机译：编织复合材料;双轴和三轴编织;数学模型;机械性能;计算机模拟;

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Development and Verification of an Analytic Technique to Determine the Stiffness Parameters of Braided Tubular Parts

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