简介概要

A simple analytical method for deflation prediction of inflatable structures

来源期刊:中南大学学报(英文版)2015年第6期

论文作者:LI Qing-song QING Qiang GONG Jing-hai

文章页码:2277 - 2286

Key words:inflatable structure; deflation; wrinkling; simulation; control volume method

Abstract: The static performance of inflatable structures has been well studied and the dynamic deployment simulation has received much attention. However, very few studies focus on its deflation behavior. Although there are several dynamic finite element algorithms that can be applied to the deflation simulation, their computation costs are expensive, especially for large scale structures. In this work, a simple method based on classic thermodynamics and the analytical relationship between air and membrane was proposed to efficiently analyze the air state variables under the condition of ventilation. Combined with failure analysis of static bearing capacity, a fast incremental analytical method was presented to predict both elastic and post wrinkling deflation process of inflatable structures. Comparisons between simplified analysis, dynamic finite element simulation, and a full-scale experimental test are presented and the suitability of this simple method for solving the air state and predicting the deflation behavior of inflatable structures is proved.

详情信息展示

A simple analytical method for deflation prediction of inflatable structures

LI Qing-song(李庆松), QING Qiang(卿强), GONG Jing-hai(龚景海)

(Department of Civil Engineering, Shanghai Jiao Tong University, Shanghai 200240, China)

Abstract:The static performance of inflatable structures has been well studied and the dynamic deployment simulation has received much attention. However, very few studies focus on its deflation behavior. Although there are several dynamic finite element algorithms that can be applied to the deflation simulation, their computation costs are expensive, especially for large scale structures. In this work, a simple method based on classic thermodynamics and the analytical relationship between air and membrane was proposed to efficiently analyze the air state variables under the condition of ventilation. Combined with failure analysis of static bearing capacity, a fast incremental analytical method was presented to predict both elastic and post wrinkling deflation process of inflatable structures. Comparisons between simplified analysis, dynamic finite element simulation, and a full-scale experimental test are presented and the suitability of this simple method for solving the air state and predicting the deflation behavior of inflatable structures is proved.

Key words:inflatable structure; deflation; wrinkling; simulation; control volume method

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