Aviation Program Group, Environmentally Compatible Airframe Technology Team, Japan Aerospace Exploration Agency (JAXA)
Aviation Program Group, Environmentally Compatible Airframe Technology Team, Japan Aerospace Exploration Agency (JAXA)
Aviation Program Group, Environmentally Compatible Airframe Technology Team, Japan Aerospace Exploration Agency (JAXA)
Foundation for Promotion of Japanese Aerospace Technology
High velocity tensile strain rate properties of four different kinds of aluminum alloys (A2024-T3clad, A7075-T6clad, A5052 and A6061) for aircraft structures are evaluated by using high rate servo-hydraulic machine at strain rates from 100 s(exp-1) to nearly 1000 s(exp-1). In this paper, tensile strength, yield strength, Young's modulus and 0.2% proof stress of aluminum alloys on various strain rates are reported. The experimental results for true stress strain diagrams on various strain rates are also compared.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
航空機用アルミニウム合金のひずみ速度依存性基本データベース
61949000.pdf
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