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http://dx.doi.org/10.5139/JKSAS.2005.33.4.035

Buckling Test and Non-linear Analysis of Aluminium Isogrid Panel  

Yoo, Joon-Tae (한국항공우주연구원 우주발사체사업단)
Lee, Jong-Woong (한국항공우주연구원 우주발사체사업단)
Yoon, Jong-Hoon (한국항공우주연구원 우주발사체사업단)
Jang, Young-Soon (한국항공우주연구원 우주발사체사업단)
Yi, Yeong-Moo (한국항공우주연구원 우주발사체사업단)
Cho, Gwang-Rae (한국항공우주연구원 우주발사체사업단)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.33, no.4, 2005 , pp. 35-40 More about this Journal
Abstract
There are many methods to reinforce the cylindrical structure for light weight design like skin-stringer and semi-monocoque. Isogrid is one of the reinforced structures to improve buckling load. Isogrid has many advantages for complex load case, internal pressure and concentrated load.In this paper, compressive buckling test and non-linear FE analysis of the isogrid panel are described. Diameter of panel is 2.4m and thickness of plate is 11.43mm. The angle which the panel accomplish is about 70 degrees and, its height is about 660mm. Local buckling, global buckling and variation of stiffness after local buckling were observed during buckling test of the panel. MSC/MARC is used for non-linear FE analysis. When analysis, initial imperfection of panel which occurred during plastic forming is considered. The results of analysis for buckling mode and buckling load have good agreements with test.
Keywords
Isogrid; Buckling; Non-linear analysis;
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