Decoupling the bending behavior and the membrane properties of finite shell elements for a correct description of the mechanical behavior of textiles with a laminate formulation

Развязывание изгибового поведения и мембранных свойств конечных оболочечных элементов для корректного описания механического поведения текстильных материалов с ламинированной формулировкой
Olaf Diestel, Chokri Cherif, Oliver Döbrich, Thomas Gereke, Sybille Krzywinski
2013-02-14

LS-DYNA implementationcantilever bending stiffnessdecoupled bending and membrane behaviordrape simulationtextile laminate formulation
Drape simulation of textiles is a field of research, which is known in the clothing sector for a long time. The ongoing development of high-performance composites made of textile reinforcements and matrix materials focus the interests on a serial production in many industrial sectors, such as aviation and automotive industries. Challenges occur mainly in the serial production technologies and in supplying concepts for the preform architecture and shape. Research aims on the acceleration of preform manufacturing and the reduction of expensive pretests. Numerical simulation models can help to improve the composite development chain with structure and process simulation. A special challenge in drape modeling is the bending behavior of textiles. This study introduces a novel approach for modeling single textile layers as laminates to gain a correct mechanical behavior, where all deformation mechanisms are uncoupled. The implementation in the finite element software LS-DYNA® is described. An algorithm is introduced which provides the membrane stiffness for each layer of a laminate to fit the measured cantilever bending stiffness of textiles in every bending direction and bending side. The calculated parameters for the laminate formulation result in the requested bending stiffness for the textile layer. The cantilever bending stiffness can be used directly for dimensioning the model.
1
Implements the laminate formulation in LS-DYNA and shows that calculated laminate parameters reproduce the requested bending stiffness of textile layers.
2
Introduces a novel laminate-based finite element approach that models single textile layers with uncoupled deformation mechanisms, enabling correct mechanical behavior.
3
Positions the method as useful for accelerating preform manufacturing and reducing expensive pretests in textile-reinforced composite production workflows.
4
Presents an algorithm that computes membrane stiffness for each laminate layer to match measured cantilever bending stiffness in all bending directions and sides.
5
States that cantilever bending stiffness can be used directly to dimension the finite element model for textile drape simulations.

Single textile layer modeled as a laminate finite shell element in LS-DYNA

Decoupling and correct representation of bending behavior and membrane properties by deriving per-layer membrane stiffness to match measured cantilever bending stiffness across bending directions/sides

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2013-02-14
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Authors
Olaf Diestel
Chokri Cherif
Oliver Döbrich
Thomas Gereke
Sybille Krzywinski
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