Buckling Analysis of Airframe Jointed Panel Under Combined Loading

The complicated relationship of the high order static indeterminate structure will lead to a lot of calculation work. The strength analysis of the structure is very difficult. In aircraft design phase, a structural simplified method should be used to model the load characteristics of the structure....

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Bibliographic Details

Published in:	International Journal of Applied Mechanics and Engineering
Main Authors:	Xu Li, Dawei Jia, Chao Meng
Format:	Article
Language:	English
Published:	University of Zielona Góra 2018-11-01
Subjects:	strength buckling analysis jointed panel combined loading
Online Access:	https://www.ijame-poland.com/Buckling-Analysis-of-Airframe-Jointed-Panel-Under-Combined-Loading,166960,0,2.html