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Modeling of the stability of a flat textile structures loaded by compression forces
By :   Piotr Szablewski
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Abstract


The aim of this paper is to examine the state of equilibrium of a flat textile structure loaded by compression forces and deadweight. Only those forms of deformed structure were considered where its two ends were supported by pivot bearings, and lie on the immovable supporting plane. Such structure may be a flat textile structure (e.g. fabric) and above-mentioned boundary conditions result directly from behavior under specified loading. In the analysis, shape of the deflection curve was determined for a given axial force and deadweight, and it was examined whether a given position is stable or unstable. Two shape parameters occurring in the analysis are used for simulation of different shapes of bending curve in the middle of compression. The analysis was made on the basis of the energetic method, by examining potential energy of the system. Results may be used for different algorithms and programs for simulation of fabric buckling, folding and for another application of textile mechanics.


1. Assumptions of model and initial equations


Let us consider a flat textile structure of length l as its longitudinal section loaded by compression force P and deadweight q as in Figure 1. The structure lies on immovable supporting plane and is supported on both ends by pivot bearings in points A and B. However, it is subject to Hooke's law while being bent, and the known relation for the bending moment is applicable to it, where is the radius of curvature, and EI means the bending rigidity. In this case, the existence of the rigid base causes the limitation of the y coordinate. It must be greater or equal to zero for each value of the arc coordinate s, which is measured along the deflection curve ().The boundary conditions for this load scheme are the following:



Let us consider the infinitesimal section of the structure presented in Figure 2. The structure is inextensible, thus. Therefore we obtain the following geometrical condition. Writing the elementary equations of equilibrium for section from Figure 3, next multiplying by the appropriate virtual displacements x, y and, adding the sides and integrating within the limits from 0 to l, we obtain


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