Introducing a discrete modelling technique for buckling of panels under combined loading

被引:0
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作者
H. A. Kim
C. A. Featherston
J. Ussel
P. A. Williams
机构
[1] University of Bath,Department of Mechanical Engineering
[2] Cardiff University,Cardiff School of Engineering
[3] Airbus UK,undefined
关键词
Stiffened panel; Buckling; Discrete model; Fast analysis model; Combined loading;
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学科分类号
摘要
The paper introduces a discrete model to describe the buckling of a stiffened panel beam under a complex loading environment. The study begins by examining the existing load interaction equation for a continuous panel. Experimental and finite element investigations establish the validity of considering the critical panel of a more complex structure in isolation. The paper then devises a discrete model for this critical panel, which was validated for a range of boundary conditions using anti-optimisation. The numerical results show that the discrete model exhibits the buckling behaviour of a continuous panel under combined loading. Recent studies established that the truss-lattice configuration has stable post-buckling behaviour and derived fast analysis technique for such a structure. It is therefore concluded that the truss-lattice model introduced in the present paper can offer a fast analysis formulation for buckling (and potentially post-buckling) of multiple-panel beams suitable for optimisation.
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页码:3 / 13
页数:10
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