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YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式
https://jaxa.repo.nii.ac.jp/records/44484
https://jaxa.repo.nii.ac.jp/records/4448415c4236f-3d46-48fc-98a5-a52767a04754
名前 / ファイル | ライセンス | アクション |
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naltr00241.pdf (3.3 MB)
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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 | YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式 | |||||
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 | Full-Scale Fatigue Test of YS-11A-500/600 Turboprop Transport Wing(I Safe-Life Fatigue Test Loads and Test Method) | |||||
著者 |
竹内, 和之
× 竹内, 和之× 野原, 利雄× 朝田, 洋雄× TAKEUCHI, Kazuyuki× NOHARA, Toshio× ASADA, Hiroo |
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著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体第一部 | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
First Airframe 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-241 巻 241, p. 23, 発行日 1971-07 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | I was required to perform the full-scale fatigue test(the safe-life and fail-safe tests) of YS-11-500/600 transport wing, because the maximum take-off weight of the aircraft was increased by 2.2 tons compared with the prototype and accordingly some strength members of the wing were re-designed. In order to perform the full-scale fatigue test, the safe-life fatigue loads and test method were investigated and the fatigue loads and program sequence of the test are decided were follows:(1)Gust loads, maneuver loads and ground-air-ground loads are taken into consideration as fatigue test loads. (2)The flight loads of one block corresponding to 100 flights are applied in an ascending-descending sequence in which ground-air-ground loads are inserted. | |||||
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: NALTR0241000 | |||||
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-241 |