Výsledky vyhledávání - "HIROSUE, Kenichi"

Wind Tunnel Investigation of an Upper Surface Blown-Flap Half Model of the NAL STOL Research Aircraft

Autor: TAKAHASHI, Hitoshi, HIROSUE, Kenichi, MIYAMOTO, Yoshito, SHIGEMI, Masashi, IWASAKI, Akihito, TAMAKI, Motoaki, ORITO, MAKIO, MORITA, YOSHIO

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-734. 734:32

An investigation has been conducted to determine the aerodynamic characteristics of the aerodynamic elements of an 8％ subsonic jet transport half model with an upper surface blowing flap system that would augment lift. Wind tunnel tests of leading

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b7a4b397b59420df62017ba5245a78a1
http://id.nii.ac.jp/1696/00044985/

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Aerodynamic Characteristics of Fan-Jet STOL Aircraft

Autor: INUMARU, Norio, TAKAHASHI, Hitoshi, HIROSUE, Kenichi, TODA, Nobuhiro, KUWANO, Naoaki

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-790. 790:99

Research on Fan-Jet STOL aircraft was initiated by NAL in 1975 as a wind-tunnel-based program aimed at the design study of experimental STOL aircraft. Aerodynamic characteristics of the Augmentor Wing type model and the Upper Surface Blowing type mod

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::dc543406d284d31ee71af40ba96bf2f7
http://id.nii.ac.jp/1696/00045042/

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Low Speed Wind Tunnel-Tests of the FA-200-XS Airplane Model Influenced with Ground Effects

Autor: HIROSUE, Kenichi, ONO, Takatugu, TAKAHASHI, Hiroshi, KUWANO, Naoaki

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-201. 201:33

資料番号: NALTR0201000
レポート番号: NAL TR-201

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c50f754eeb1b5357efd858c1f34d2043
http://id.nii.ac.jp/1696/00044438/

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Design and Development of the Gust Wind Tunnel at the National Aerospace Laboratory

Autor: HIROSUE, Kenichi, KITAMURA, Kiyomi, MURAKAMI, Yoshitaka, SHINDO, Shigemi

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-335. 335:27

資料番号: NALTR0335000
レポート番号: NAL TR-335

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6d86765ed9785012694b6588e5922f31
http://id.nii.ac.jp/1696/00044575/

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