Analysis of Gossamer Structures Using Assumed-Strain Solid-Shell Finite Elements

The objective of this study is to investigate the applicability of assumed-strain solid-shell finite elements for analysis of gossamer space and near-space structures such as solar sails and scientific balloons. The solid-shell element formulation that alleviates the element locking via the assumed-strain approach has been successfully used for analysis of extremely thin structures. In this study, quadruple precision is explored to further extend the capability of the nine-node assumed-strain solid-shell elements to analyses of extremely thin structures. As examples, geometrically nonlinear static analyses of solar sail ribbons and a square membrane are carried out, without using any stabilizing scheme. Subsequently, the assumed-strain solid-shell element formulation with quadruple precision are successfully used to determine the deformed shape and the stress distribution of a scientific balloon at various altitudes.