Failure Mode Analysis Of Kagome Lattice Structures
Ultralight weight structures are today’s essential need in aerospace, marine and automotive industries. Strength and stiffness optimization of load bearing structures is made possible with the evolution of additive manufacturing technologies through shape or topology optimization. Further composite...
Saved in:
Main Authors: | , , |
---|---|
Other Authors: | |
Format: | Conference or Workshop Item |
Language: | English |
Published: |
2016
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/84555 http://hdl.handle.net/10220/41847 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
id |
sg-ntu-dr.10356-84555 |
---|---|
record_format |
dspace |
spelling |
sg-ntu-dr.10356-845552020-09-24T20:11:50Z Failure Mode Analysis Of Kagome Lattice Structures Rinoj, Gautam Idapalapati, Sridhar Feih, Stefanie School of Mechanical and Aerospace Engineering Proceedings of the 2nd International Conference on Progress in Additive Manufacturing (Pro-AM 2016) A*STAR SIMTech Singapore Centre for 3D Printing Kagome structures Fused deposition modelling Ultralight weight structures are today’s essential need in aerospace, marine and automotive industries. Strength and stiffness optimization of load bearing structures is made possible with the evolution of additive manufacturing technologies through shape or topology optimization. Further composite materials and sandwich constructions reduce the design weight. To fully realize the lightweight structure, core designs with low density and high strength are necessary for sandwich panel design. In this study, the performance of the 3D Kagome truss core structure in compression loading is experimentally investigated. These bio-inspired core structures are fabricated by Fused Deposition Modelling (FDM) with Acrylonitrile butadiene styrene (ABS) ABSplus® material for experimental validation purposes. The geometrical parameters of the Kagome structure in terms of its slenderness ratio are varied to study the switch of failure mechanism from yielding dominant behavior to buckling. The effective stiffness of the truss found from finite element modeling and based on experimental results are compared, and the reasons for their discrepancy are explored. The modulus of the Kagome unit-cell is found to be linearly related to its relative density. The result show that with the increase in the slenderness ratio (l/r), the strength of the Kagome structure decreases. MOE (Min. of Education, S’pore) Published version 2016-12-13T09:12:16Z 2019-12-06T15:47:08Z 2016-12-13T09:12:16Z 2019-12-06T15:47:08Z 2016 Conference Paper Rinoj, G., Idapalapati, S., & Feih, S. (2016). Failure Mode Analysis Of Kagome Lattice Structures. Proceedings of the 2nd International Conference on Progress in Additive Manufacturing (Pro-AM 2016), 91-96. https://hdl.handle.net/10356/84555 http://hdl.handle.net/10220/41847 en © 2016 by Pro-AM 2016 Organizers. Published by Research Publishing, Singapore 6 p. application/pdf |
institution |
Nanyang Technological University |
building |
NTU Library |
country |
Singapore |
collection |
DR-NTU |
language |
English |
topic |
Kagome structures Fused deposition modelling |
spellingShingle |
Kagome structures Fused deposition modelling Rinoj, Gautam Idapalapati, Sridhar Feih, Stefanie Failure Mode Analysis Of Kagome Lattice Structures |
description |
Ultralight weight structures are today’s essential need in aerospace, marine and automotive industries. Strength and stiffness optimization of load bearing structures is made possible with the evolution of additive manufacturing technologies through shape or topology optimization. Further composite materials and sandwich constructions reduce the design weight. To fully realize the lightweight structure, core designs with low density and high strength are necessary for sandwich panel design. In this study, the performance of the 3D Kagome truss core structure in compression loading is experimentally investigated. These bio-inspired core structures are fabricated by Fused Deposition Modelling (FDM) with Acrylonitrile butadiene styrene (ABS) ABSplus® material for experimental validation purposes. The geometrical parameters of the Kagome structure in terms of its slenderness ratio are varied to study the switch of failure mechanism from yielding dominant behavior to buckling. The effective stiffness of the truss found from finite element modeling and based on experimental results are compared, and the reasons for their discrepancy are explored. The modulus of the Kagome unit-cell is found to be linearly related to its relative density. The result show that with the increase in the slenderness ratio (l/r), the strength of the Kagome structure decreases. |
author2 |
School of Mechanical and Aerospace Engineering |
author_facet |
School of Mechanical and Aerospace Engineering Rinoj, Gautam Idapalapati, Sridhar Feih, Stefanie |
format |
Conference or Workshop Item |
author |
Rinoj, Gautam Idapalapati, Sridhar Feih, Stefanie |
author_sort |
Rinoj, Gautam |
title |
Failure Mode Analysis Of Kagome Lattice Structures |
title_short |
Failure Mode Analysis Of Kagome Lattice Structures |
title_full |
Failure Mode Analysis Of Kagome Lattice Structures |
title_fullStr |
Failure Mode Analysis Of Kagome Lattice Structures |
title_full_unstemmed |
Failure Mode Analysis Of Kagome Lattice Structures |
title_sort |
failure mode analysis of kagome lattice structures |
publishDate |
2016 |
url |
https://hdl.handle.net/10356/84555 http://hdl.handle.net/10220/41847 |
_version_ |
1681057214771494912 |