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Buckling analysis of airframe jointed panel under combined loading

Li X., Jia D., Meng C.

International Journal of Applied Mechanics and Engineering

2018

Vol. 23, no. 4

1035--1042

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. In the paper, the buckling analysis of airframe jointed panel is investigated under combined loading and the effect of jointed position to buckling load is also presented. For the buckling analysis of special joined structure, one new method which is better than traditional methods is described.