Wrinkle-crease interaction behavior simulation of a rectangular membrane under shearing
查看参考文献28篇
文摘
|
Wrinkling analysis of a rectangular membrane with a single crease under shearing is performed to understand the wrinkle-crease interaction behaviors.The crease is considered by introducing the residual stresses from creasing and the effective modulus into the baseline configuration with assumed circular cross-sectional crease geometry.The wrinkling analysis of the creased membrane is then performed by using the direct perturb-force(DP)simulation technique which is based on our modified displacement components(MDC)method.Results reveal that the crease may influence the stress transfer path in the membrane and further change the wrinkling direction.The crease appears to improve the bending stiffness of the membrane which has an effective resistance on the wrinkling evolution.The effects of the crease orientation on wrinkle-crease interaction are studied toward the end of this paper.The results show that the wrinkling amplitude,wavelength,and direction increase as the crease orientation increases,and the wrinkling number decreases with the increasing crease orientation.These results will be of great benefit to the analysis and the control of the wrinkles in the membrane structures. |
来源
|
Acta Mechanica Sinica
,2011,27(4):550-558 【核心库】
|
DOI
|
10.1007/s10409-011-0473-5
|
关键词
|
Membrane structure
;
Wrinkle-crease interaction
;
Membrane wrinkling
;
Creased membrane
|
地址
|
1.
Center for Composite Materials,Harbin Institute of Technology, Harbin, 150001
2.
Center for Composite Materials,Harbin Institute of Technology, Harbin, 150080
|
语种
|
英文 |
文献类型
|
研究性论文 |
ISSN
|
0567-7718 |
学科
|
力学 |
基金
|
国家自然科学基金
;
国家教育部高等学校博士学科点专项科研基金
;
中国航空科学基金
;
Fundamental Research Funds for the Central Universities
|
文献收藏号
|
CSCD:4313304
|
参考文献 共
28
共2页
|
1.
Jenkins,C.H. Gossamer spacecraft:membrane and inflatable structures technology for space applications.
In:Progress in Astronautics and Aeronautics,Vol.191,2001:103-105
|
CSCD被引
1
次
|
|
|
|
2.
Jenkins,C.H. Gossamer spacecraft:membrane and inflatable structures technology for space applications.
In:Progress in Astronautics and Aeronautics,Vol.191,2001:321-331
|
CSCD被引
1
次
|
|
|
|
3.
Jenkins,C.H. Recent advances in gossamer spacecraft:Chapter 3 membrane wrinkling.
In:Progress in Astronautics and Aeronautics,Vol.212,2006:109-164
|
CSCD被引
1
次
|
|
|
|
4.
Miller R K. Finite element analysis of partly wrinkled membranes.
Comp.&Struc,1985,20(3):631-639
|
CSCD被引
10
次
|
|
|
|
5.
Pipkin A C. The relaxed energy density for isotropic elastic membranes.
IMA J.Appl.Math,1986,36(1):85-99
|
CSCD被引
2
次
|
|
|
|
6.
Liu X. Fine scale analysis of wrinkled membrane.
Int.J.Comput.Eng.Sci,2000,1(2):281-298
|
CSCD被引
1
次
|
|
|
|
7.
Ding H. The modeling and numerical analysis of wrinkled membranes.
Int.J.Numer.Meth.Eng,2003,58(12):1785-1801
|
CSCD被引
19
次
|
|
|
|
8.
Coman C D. On the applicability of tension field theory to a wrinkling instability problem.
Acta Mechanica,2007,190(1/4):57-72
|
CSCD被引
1
次
|
|
|
|
9.
Jarasjarungkiat A. A wrinkling model based on material modification for isotropic and orthotropic membranes.
Comput.Methods Appl.Mech.Engrg,2008,197(6/8):773-788
|
CSCD被引
5
次
|
|
|
|
10.
Leifer,J. Prediction of wrinkle amplitudes in thin film membranes using finite element modeling.
In:Proc.of the 44th AIAA/ASME/ASCE/AHS Structures,Structural Dynamics,and Materials Conference,7-10 April,Norfolk,Virginia.AIAA 2003-1983,2003
|
CSCD被引
1
次
|
|
|
|
11.
Wong Y. Wrinkled membrane,part I:experiments;part II:analytical models;part III:numerical simulations.
J.Mech.Mater.Struct,2006,1(1):3-95
|
CSCD被引
2
次
|
|
|
|
12.
Tessler A. Geometrically nonlinear shell analysis of wrinkled thin-film membranes with stress concentrations.
J.Spacecraft Rockets,2007,44(3):582-588
|
CSCD被引
2
次
|
|
|
|
13.
Wang C G. Wrinkling prediction of rectangular shell-membrane under transverse in-plane displacement.
Int.J.Solids Structures,2007,44(20):6507-6516
|
CSCD被引
10
次
|
|
|
|
14.
Wang C G. Wrinkling behaviors of gossamer structure with stretched annulus-shape under in-plane torsion.
Mech.Adv.Mater.Struc,2008,15(2):157-164
|
CSCD被引
1
次
|
|
|
|
15.
Wang C G. A new computational method for wrinkling analysis of gossamer space structures.
Int.J.Solids Structures,2009,46(6):1516-1526
|
CSCD被引
10
次
|
|
|
|
16.
Wang,J.T. Simulating nonlinear deformations of solar sail membranes using explicit time integration.
In:Proc.of 45th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference,,Palm Springs,CA,AIAA 2004-1580,2004
|
CSCD被引
1
次
|
|
|
|
17.
Wang C G. Numerical simulation of wrinkles in space inflatable structures.
J.Spacecraft Rockets,2006,43(5):1146-1149
|
CSCD被引
5
次
|
|
|
|
18.
Murphey,T.W.
A nonlinear elastic constitutive model for wrinkled thin films.[Ph.D.Thesis],2000:1-133
|
CSCD被引
1
次
|
|
|
|
19.
MacNeal R.
Tensile properties of a tape with a transverse crease,Astro Research Corporation,Rept.ARC-R-241,1966:1-14
|
CSCD被引
1
次
|
|
|
|
20.
Gough,A. Experimental and numerical study of creased membranes.
In:Proc.of 46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference Apr,AIAA 2005-1976,2005
|
CSCD被引
1
次
|
|
|
|
|