Effects of Radial Inertia and End Friction in Specimen Geometry in Split Hopkinson Pressure Bar Tests : A Computational Study
Mechanics of Materials 51 巻
97-109 頁
2012 発行
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MechMat_51_97.pdf
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タイトル ( eng ) |
Effects of Radial Inertia and End Friction in Specimen Geometry in Split Hopkinson Pressure Bar Tests : A Computational Study
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作成者 |
Yokoyama Takashi
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収録物名 |
Mechanics of Materials
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巻 | 51 |
開始ページ | 97 |
終了ページ | 109 |
抄録 |
The split Hopkinson pressure bar (SHPB) technique has been used widely for the impact testing of materials in the strain-rate range from 10(2) to 10(4) s(-1). However, some specific problems still remain mainly concerning the effects of radial inertia and end friction in a cylindrical specimen on the accurate determination of dynamic stress-strain curves of materials. In this study, the basic principle of the SHPB technique is revisited based on energy conservation and some modifications are made considering radial momentum conservation. It is pointed out that the radial inertia and end friction effects are coupled to each other in the SHPB specimen. Computational simulations using the commercial finite element (FE) code ABAQUS/Explicit ver. 6.8 are conducted to check the validity of the modifications for ductile pure aluminum specimens. Both rate-independent and rate-dependent models are adopted for the test material. Simulations are performed by varying two different control parameters: a friction coefficient between the specimen and the pressure bars and a slenderness ratio of the specimen (or thickness to diameter ratio).
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著者キーワード |
Finite elements
Impact compression
Elastoplasticity
Viscoplastic response
Split Hopkinson pressure bar
Radial inertia
End friction
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NDC分類 |
機械工学 [ 530 ]
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言語 |
英語
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資源タイプ | 学術雑誌論文 |
出版者 |
Elsevier B.V.
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発行日 | 2012 |
権利情報 |
(c) 2012 Elsevier B.V. All rights reserved.
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出版タイプ | Author’s Original(十分な品質であるとして、著者から正式な査読に提出される版) |
アクセス権 | オープンアクセス |
収録物識別子 |
[ISSN] 0167-6636
[DOI] 10.1016/j.mechmat.2012.04.007
[NCID] AA1063514X
[DOI] http://dx.doi.org/10.1016/j.mechmat.2012.04.007
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