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某飞行器复合材料薄壁加筋结构舱段稳定性分析

刘文一 焦冀光

舰船电子工程Issue(2):110-113,4.
舰船电子工程Issue(2):110-113,4.DOI:10.3969/j.issn.1672-9730.2016.02.030

某飞行器复合材料薄壁加筋结构舱段稳定性分析

Stability Analysis of A Aircraft's Thin-walled Reinforced Composite Material Cabin

刘文一 1焦冀光1

作者信息

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摘要

Abstract

The finite element method has been used to study the stability of thin‐walled reinforced composite material cabin under a particular cabin load .The change behavior of cabin stability has been find when the rib's height has been changed as it's was 200mm2 ,300mm2 and 400mm2 ,though the thickness of the thin wall was constant .the critical load has been figured out ,the results could be used as reference for engineering design .

关键词

舱段/屈曲/有限元法

Key words

cabin/bulking/finite element method

分类

航空航天

引用本文复制引用

刘文一,焦冀光..某飞行器复合材料薄壁加筋结构舱段稳定性分析[J].舰船电子工程,2016,(2):110-113,4.

舰船电子工程

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1672-9730

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