Article ID Journal Published Year Pages File Type
498306 Computer Methods in Applied Mechanics and Engineering 2012 12 Pages PDF
Abstract

This paper discusses the evaluation of quasi-static equilibrium solutions for inflatable space membrane structures. A Mooney–Rivlin hyper-elastic material model, with variable constitutive constants, is considered. A compressible weightless medium is used to introduce within the membrane a one-parametric over-pressure loading compared to an ambient pressure. Analytical instability results are shown for a spherical and derived for a cylindrical case. These are compared to numerical simulations based on a flat linearly interpolated triangular space membrane element. Path-following procedures are used to find generalized equilibrium paths, with different parameterizations. Numerical examples show that the methods developed can give information on the stability of the membranes, but that the medium and means for introducing the internal pressure are of importance for the interpretation of stability.

► We study the inflation of thin space membranes subjected to internal over-pressure. ► We use both analytical and FE methods for the balloon studies. ► We study the instability behavior with respect to the loading mechanism. ► Numerical simulations are based on a simple 3D element. ► The simulation of all instabilities demand sophisticated path-following.

Related Topics
Physical Sciences and Engineering Computer Science Computer Science Applications
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