Zobrazeno 1 - 10 of 17 pro vyhledávání: '"Yoshimoto, Norio"'
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Akademický článek
Unsteady transonic aerodynamics during wing flutter
Autor: Saitoh Kenichi, Tamayama Masato, Yoshimoto Norio, Ueda Tetsuhiko
Publikováno v: Open Engineering, Vol 2, Iss 3, Pp 410-417 (2012)
Externí odkaz: https://doaj.org/article/db52f7f4767c40a4a008f234781c2818
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3
Effect of vibration data preprocessing for flutter margin prediction
Autor: Tamayama, Masato, Saitoh, Kenichi, Yoshimoto, Norio, Arizono, Hitoshi
Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of the First International Symposium on Flutter and its Application. :97-104
First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan
Although airplane's model certification must be proved by showing enough damping margin at every flight condition, the damp
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b35193fe9f4f9556321511b3c2cf4b16
http://id.nii.ac.jp/1696/00003396/
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6
Vertical drop impact test of a YS-11 fuselage section
Autor: Kumakura, Ikuo, Minegishi, Masakatsu, Iwasaki, Kazuo, Shoji, Hirokazu, Yoshimoto, Norio, Miyaki, Hiromitsu, Sashikuma, Hirofumi, Isoe, Akira, Yamaoka, Toshihiro, Katayama, Noriaki
Publikováno v: 航空宇宙技術研究所特別資料: 平成14年度航空安全・環境適合技術研究研究交流会と研究報告会講演論文集 = Special Publication of National Aerospace Laboratory: Proceedings of the Information Exchange Meeting and the Research Meeting on Aviation Safety and Environmental Compatibility Technology Research FY2001. 55:79-82
資料番号: AA0045946005
レポート番号: NAL SP-55
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::57b5c54cb966f2f36daf4100aa6dfae5
http://id.nii.ac.jp/1696/00038179/
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7
Evaluation Tests for Flutter Wind Tunnel Flow Accuracy
Autor: Tamayama, Masato, Saito, Kenichi, Arizono, Hitoshi, Yoshimoto, Norio, Kikuchi, Takao
Publikováno v: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum.
遷音速フラッタ試験設備は昭和34年の設備完成当時に気流の確認試験を行った．その後，平成5 - 8年に実施した圧力制御系の改修に伴ってその改修仕様確認の試験を簡単に実施したが，包
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6fc7656dbad1e44ebbc8f939893b2d44
http://id.nii.ac.jp/1696/00002575/
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8
Vertical drop test of a YS-11 fuselage section(Part 2)
Autor: Iwasaki, Kazuo, Minegishi, Masakatsu, Shoji, Hirokazu, Miyaki, Hiromitsu, Yoshimoto, Norio, Terada, Hiroyuki, Kumakura, Ikuo, Katayama, Noriaki, Hayashi, Toru, Kosaka, Hideyuki
Publikováno v: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report.
The Structures and Materials Research Center of the National Aerospace Laboratory of Japan (NAL) in conjunction with Kawasaki Heavy Industries, LTD (KHI) conducted a second vertical drop test of a fuselage section cut from a NAMC YS-11 transport airp
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::76e50aed1824755cd3992b7a772f3bde
http://id.nii.ac.jp/1696/00002404/
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9
Vertical drop test of a YS-11 fuselage section(Part1)
Autor: Minegishi, Masakatsu, Iwasaki, Kazuo, Kumakura, Ikuo, Shoji, Hirokazu, Yoshimoto, Norio, Terada, Hiroyuki, Sashikuma, Hirofumi, Isoe, Akira, Yamaoka, Toshihiro, Katayama, Noriaki
Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1461
The Structures and Materials Research Center of the National Aerospace Laboratory of Japan(NAL) and Kawasaki Heavy Industries, Ltd.(KHI) conducted a vertical drop test of a fuselage section cut from a NAMC YS-11 transport airplane at the NAL vertical
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::25d3845de83a90049fe97fa8b25542f3
http://id.nii.ac.jp/1696/00042857/
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