Creator:

Xu Li ; Dawei Jia ; Chao Meng

Contributor:

Jurczak, Paweł - red.

Title:

Buckling analysis of airframe jointed panel under combined loading

Group publication title:

IJAME, volume 23 (2018)

Subject and Keywords:

strength ; buckling analysis ; jointed panel ; combined loading

Abstract:

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.

Publisher:

Zielona Góra: Uniwersytet Zielonogórski

Date:

2018

Resource Type:

artykuł

Format:

application/pdf

DOI:

10.2478/ijame-2018-0060

Pages:

1035-1042

Source:

IJAME, volume 23, number 4 (2018)

Language:

eng

License:

CC 4.0

License CC BY-NC-ND 4.0:

click here to follow the link

Rights:

Biblioteka Uniwersytetu Zielonogórskiego