首页 | 本学科首页   官方微博 | 高级检索  
     

斜削型筋条复合材料加筋壁板轴压屈曲分析
引用本文:赵铭,张伟,王鹏飞. 斜削型筋条复合材料加筋壁板轴压屈曲分析[J]. 科学技术与工程, 2017, 17(6)
作者姓名:赵铭  张伟  王鹏飞
作者单位:中国特种飞行器研究所,中国特种飞行器研究所,中国特种飞行器研究所
摘    要:复合材料加筋壁板大量应用在飞机结构中而斜削型筋条加筋壁板由于其特殊的偏心结构使得其与常规的贯通型筋条加筋壁板有着不一样的屈曲载荷。以斜削型筋条复材加筋壁板为例,通过试验、工程算法、有限元法三种方法对其屈曲模式进行分析对比分析三种方法所得结果,得出斜削型筋条对加筋壁板屈曲载荷的削弱作用在30%左右,工程算法保守量为11%左右。

关 键 词:加筋壁板  屈曲  试验  工程算法  有限元
收稿时间:2016-08-30
修稿时间:2016-08-30

An analysis of buckling modes in composite panel with beveled stiffened under compress load
Zhao Ming,Zhang Wei and Wang Pengfei. An analysis of buckling modes in composite panel with beveled stiffened under compress load[J]. Science Technology and Engineering, 2017, 17(6)
Authors:Zhao Ming  Zhang Wei  Wang Pengfei
Abstract:Composite stiffened panel is widely used in aircraft structure. Whereas, the panel with beveled stiffened because of the especial eccentric structure has a different buckling load from the conventional composite panel. This paper takes composite panel with beveled stiffened for an example, analyzes the buckling modes via three methods-testing, engineering methods and finite element method, and evaluates the effect of beveled stiffened on buckling load. By comparing the three methods, the conservative quantity of the engineering methods is given, which provided the testing and analysis method for the buckling analysis of the composite stiffened panel.
Keywords:stiffened panels  buckling  test  engineering methods  finite elements
本文献已被 CNKI 等数据库收录!
点击此处可从《科学技术与工程》浏览原始摘要信息
点击此处可从《科学技术与工程》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号