scholarly journals Morphing of curved corrugated shells

2009 ◽  
Vol 46 (7-8) ◽  
pp. 1624-1633 ◽  
Author(s):  
A.D. Norman ◽  
K.A. Seffen ◽  
S.D. Guest
Keyword(s):  
ce/papers ◽  
2021 ◽  
Vol 4 (2-4) ◽  
pp. 1829-1836
Author(s):  
Ruizhi Zhang ◽  
Leroy Gardner ◽  
Xin Meng ◽  
Craig Buchanan ◽  
Ville‐Pekka Matilainen ◽  
...  

2011 ◽  
Vol 46 (9) ◽  
pp. 1001-1009 ◽  
Author(s):  
I. Yu. Babich ◽  
N. B. Zhukova ◽  
N. P. Semenyuk ◽  
V. M. Trach

Author(s):  
A.D Norman ◽  
K.A Seffen ◽  
S.D Guest

We have been constructing and investigating multistable corrugated shell structures. The multistability arises from the interaction between internal prestresses created during forming and nonlinear geometrical changes during deformation. Using a simplified analytical elastic model, we homogenize the properties of the shells through simultaneously considering the material on two scales: the ‘local’ scale of the isotropic material; and the ‘global’ scale of the corrugated sheet, which is then modelled as an equivalent flat sheet with anisotropic properties. This model is applied to simulate two modes of bistability observed in prototypes: first, prestressed corrugated shells that, when buckled, can coil up into a tube repeatably and reversibly; and second, corrugated sheets with a symmetry-breaking ‘twisting’ curvature. The model gives an intuitive understanding of the behaviour, and has enabled us to understand forming processes that give the behaviour we wish, including tristable shells that combine both bistable modes.


2018 ◽  
Vol 931 ◽  
pp. 3-8 ◽  
Author(s):  
Eduard G. Yanukyan ◽  
Anton Chepurnenko ◽  
Batyr M. Yazyev ◽  
Michael S. Turko

The method of calculating the shells of revolution for an asymmetric load using a semi-analytic finite element method is considered. An example is given of calculating a corrugated cylindrical tank for wind load. Comparison of meridional and annular forces is performed for a smooth and corrugated shell of identical dimensions.


Thin Shells ◽  
1980 ◽  
pp. 271-284
Author(s):  
J.E. GIBSON
Keyword(s):  

1967 ◽  
Vol 1 (4) ◽  
pp. 382-388 ◽  
Author(s):  
Harold G. Franklin

A membrane solution of fiber-reinforced corrugated shells of revolution under axial and torsional loading is determined from the equations of a thin shell whose middle surface is referred to an orthogonal coordinate system. Explicit formulas for the stress resultants are determined and the displacements are stated in terms of simple quadratures without specifying the shape of the profile of the shell. It is found that the displacements are coupled under both loading conditions except when the orientation of the fibers are at the two extremes.


1976 ◽  
Vol 102 (10) ◽  
pp. 2033-2051
Author(s):  
Herbert A. Mang ◽  
C. V. Girÿa Vallabhan ◽  
Jimmy H. Smith

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