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<論文>アルミ黄銅,チタン銅合金,キュプロ・ニッケルの圧延板のたわみの塑性
https://jaxa.repo.nii.ac.jp/records/31456
https://jaxa.repo.nii.ac.jp/records/3145638b97751-95ce-407a-9747-45423a9c755d
名前 / ファイル | ライセンス | アクション |
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SA0124338.pdf (1.7 MB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | <論文>アルミ黄銅,チタン銅合金,キュプロ・ニッケルの圧延板のたわみの塑性 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Bending Plasticity of Strips of Aluminum-brass, Copper-titanium Alloy and Cupro-nickel | |||||
著者 |
村川, 洯
× 村川, 洯× 松岡, 輝雄× MURAKAWA, Kiyoshi× MATSUOKA, Teruo |
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著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 1, 号 2, p. 59-68, 発行日 1965-04 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | アルミ黄銅,チタン銅合金およびキュプロ・ニッケルの圧延板に低温焼鈍をほどこすことのたわみの塑性(K_b)におよぼす影響をしらべた.ここでしらべたキュプロニッケルは20% Niを含有していて,もしその他に2%以上のAlを含有する場合には適当な熱処理をほどこせば時効硬化を示すことがわかった. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Bending plasticity (K_b) of strips of aluminum-brass, copper-titanium, alloy and cupro-nickel that were cold-rolled and then given low-temperature anneal was measured. The cupro-nickel sample that was tested in the present work contained approximately 20% Ni; the sample that contained more than 2% Al in addition to 20 % Ni showed age-hardening when properly heated-treated. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0124338000 |