Abstract The equilibrium between the rods and panels in the ribbed shells is considered based on the total system of structural mechanics equations as applied to a discrete model. Also shown is an approach to solving the problems that permits the stiffness matrix of shear panels to be obtained with regard for the equilibrium along the boundary with rods. The connection with the standard hybrid method of constructing stiffness matrices is indicated. The solutions for separate elements and examples illustrating the approach being proposed are presented.
The principle of constructing a computation model of equilibrium ribbed stiffened shells in linear displacement-based FEM analysis
Russian Aeronautics (Iz VUZ) ; 56 , 2 ; 117-125
2013-04-01
9 pages
Article (Journal)
Electronic Resource
English
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