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NASA NTRS · 20205010745

Multiscale Simulation of Deployable Composite Structures

Yufei Long·Orzuri Rique Garaizar·Juan M. Fernandez·Andrew C. Bergan·Wenbin Yu
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Abstract

In this paper, a multiscale simulation method for analyzing deployable composite structures is presented. Effective shell properties of the composites are obtained based on Mechanics of Structure Genome (MSG) homogenization, and then implemented into a user-subroutine UGENS for structural simulation with shell elements in Abaqus. The column bending test(CBT) of a flat thin flexure and lenticular composite boom in a simplified deployer structure are studied for demonstration. A viscoelastic material model with direct integration is adopted in this paper. The CBT simulation shows good agreement with experiments during relaxation, while errors are observed when comparing residual deformation. It is shown that this CBT model can be calibrated to CBT test results. For the lenticular boom analysis, the complete process of flattening, coiling, stowage, deployment and recovery is simulated with the viscoelastic shell model.

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Finite element analysisMechanics of Structure Genomedeployable structureshomogenizationmulti-scale composite modeling

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Yufei Long, Orzuri Rique Garaizar, Juan M. Fernandez, Andrew C. Bergan, Wenbin Yu. Multiscale Simulation of Deployable Composite Structures. https://ntrs.nasa.gov/citations/20205010745

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