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Wrinkles in Square Membranes 117<br />

following a similar approach [13], to obtain the following expressions for halfwavelength<br />

and amplitude<br />

<br />

and<br />

λ =<br />

4 2π2R1(R1 − r1) 2Et3 sin θ1<br />

3(1 − ν2 )T1 T<br />

(23)<br />

A = 2λ(δ1 + δ2)<br />

π<br />

(24)<br />

Here δ1 and δ2 are the radial displacements of the corners loaded by T1 T and<br />

T2 T , respectively; these corner displacements can be estimated from<br />

δi ≈<br />

Ti T<br />

<br />

θi ln Ri<br />

<br />

Ai<br />

+(1− ν) + θi − 1<br />

<br />

tan θi<br />

2<br />

i = 1, 2 (25)<br />

2Etsin 2 θi<br />

r1<br />

Here, Ai is theareaofapartofthe central, biaxially stressed region that is<br />

associated with the loads Ti T . More refined estimates can be obtained from a<br />

two-dimensional finite-element analysis, see Section 5.<br />

4 Finite-Element Simulations<br />

We have recently shown [14] that wrinkling of a thin membrane can be accurately<br />

modelled using the thin shell elements available in the commercial<br />

finite-element package ABAQUS [15]. The analysis is carried out by introducing<br />

initial geometrical imperfections, obtained from an initial eigenvalue<br />

analysis, followed by a geometrically non-linear post-buckling analysis using<br />

the pseudo-dynamic *STABILIZE solution scheme. This approach, although<br />

expensive in computational terms, is so far the only method that can reveal<br />

full wrinkle details and can be relied upon as an almost exact replication of<br />

physical experimentation. An alternative approach is the Iterative Modified<br />

Properties (IMP) method [9] which uses a combined stress-strain wrinkling<br />

criterion inatwo-dimensional membrane model. The IMP method has been<br />

recently implemented as an ABAQUS user subroutine and has been shown to<br />

accurately predict the extent of the wrinkled regions and the two-dimensional<br />

stress distribution —but of course not the details ofthe wrinkles.<br />

Both of these modelling techniques were used to simulate a 0.025 mm thick,<br />

500×500 mm 2 square Kapton membrane (E=3530 N/mm 2 and ν =0.3). The<br />

membrane was loaded at each corner through a spreader beam by a 0.1 mm<br />

thick, 25 mm × 20 mmKapton tabs—as in the experiment of Section 2.<br />

A uniform mesh of 200 by 200 square elements was used to model the<br />

whole structure, in order to capture the fine wrinkle details in the corners.<br />

In the shell model, the Kapton membrane and the corner tabs were modelled<br />

using S4R5 thin shell elements of different thickness. At the corners, the<br />

shell elements were connected to “Circ” beam elements through the *MPC,<br />

R 2 i

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