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多数の偏心円孔を有する回転円板の応力(有限要素法による計算)
https://jaxa.repo.nii.ac.jp/records/44638
https://jaxa.repo.nii.ac.jp/records/4463864e49014-a944-4057-81a7-af80f0969113
名前 / ファイル | ライセンス | アクション |
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naltr00390.pdf (762.4 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 多数の偏心円孔を有する回転円板の応力(有限要素法による計算) | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Stresses in a Rotating Disk with a Central and Noncentral Holes(Stress Analysis by The Finite Element Method) | |||||
著者 |
松末, 勝利
× 松末, 勝利× 長松, 昭男× 橋本, 良作× 米内山, 誠× MATSUSUE, Katsutoshi× NAGAMATSU, Akio× HASHIMOTO, Ryosaku× YONAIYAMA, Makoto |
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著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
東京工業大学 | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
東京都立航空工業高等専門学校 | ||||||
著者所属 | ||||||
元・航空宇宙技術研究所原動機部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan College of Aeronautical Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Former Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-390 巻 390, p. 12, 発行日 1974-10 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Stresses on peripheries of holes in a rotating disk with a central and noncentral holes are calculated by the finite element method in order to discuss the strength of the disk when the additional centrifugal force acts on the circumference of the disk. As the results of the present calculations, followings are pointed out, 1.Figures of stress distribution in the disk are affected by the position, the diameter and the number of the noncentral holes as well as the centrifugal force on the circumference of the disk, 2.The optimum condition which gives the smallest value of the maximum stress at the disk periphery is decided by the proper selection of the position, the diameter and the number of the noncentral holes for a given disk, and 3.The minimum of the stress concentration factor at the hole periphery, which is attainable for a given disk, can well be estimated by introducing a length ratio(total hole diameter to the peripheral length of the circle along the centers of the holes). | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0390000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-390 |