کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5472813 1520067 2017 11 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Deployment simulation of foldable origami membrane structures
ترجمه فارسی عنوان
شبیه سازی انعطاف پذیر از سازه های غشایی اریگامی هماهنگ
کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی

In recent years, with the development of the space structures, thin film reflector structures have the feature of lightweight, high compact ratio, easy to fold and unfold and so on. Its form has received wide attention from researchers and a broad application prospect. In this paper, the nonlinear finite element software ABAQUS was used to carry out the numerical simulation of the deployment of membrane structures based on Miura-ori, by taking advantage of the variable Poisson's ratio model to revise the stress distribution of membrane elements. Then the uniaxial tension tests were carried out to study the material properties of the polyimide film. The effective elastic modulus was used to simulate the crease of the membrane. The deployment of a membrane structure based on Miura origami pattern was studied. Moreover, effects of some parameters, such as the number of loading nodes and the loading rate on the numerical results were discussed.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 67, August 2017, Pages 343-353
نویسندگان
, , , , , ,