年次大会講演論文集
Online ISSN : 2433-1325
セッションID: 1461
会議情報
1461 航空機の衝撃安全シミュレータ開発のための材料特性評価の試み(S20-4 衝突現象の評価,S20 実験力学的手法による材料・製品の評価)
佐藤 裕久阿部 晃久中野 友彦細矢 大嗣岡戸 陽子鈴木 祐也
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会議録・要旨集 認証あり

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Stress-strain curves of commercially pure aluminum (JIS: A1100-H14) and super duralumin (JIS: A2024-T3) are determined in a wide range of strain rates under conditions of uniaxial strain. The plate impact testing with three in-material gauges is used to measure stress wavefronts and the UWSS is also used to derive various variables. The phase velocity of stress are determined on considering the effect of thickness of the gauges. For the low strain rate of ca. 1/10^4 [1/s] the stress-strain curves are determined under conditions of uniaxial stress by the universal testing machine combined with an extrapolation procedure. It is approximately shown that the stress is independent of strain-rate in a wide range under conditions of uniaxial strain for these light metals.

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