Výsledky vyhledávání - "空力負荷"

Design verification of H-2A auxiliary engine support structure and transonic wind tunnel test

Autor: Kanda, Atsushi, Kai, Takashi, Suito, Takanobu, Nakamichi, Jiro

Publikováno v: 宇宙航空研究開発機構特別資料: 第67回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 67th Meeting. :9-13

NAL (National Aerospace Laboratory of Japan) cooperates with NASDA (National Space Development Agency of Japan) to verify the design of the H-2A Auxiliary Engine Support Structures that are located between SSBs of the H-2A launch vehicle No.2. It is

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::151212dbd27ad4cc6471633761283b30
http://id.nii.ac.jp/1696/00006580/

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On the design issues of a stratospheric platform airship structure

Autor: Maekawa, Shoji

Publikováno v: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 772

通信技術の発達に伴って、成層圏プラットフォームとしての飛行船の可能性が注目されている。飛行船は19世紀後半に発明され、第1次世界大戦前後に大飛躍を遂げたが、固定翼航空機の�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e083f2027f2422a61d38110d2b8643bd
http://id.nii.ac.jp/1696/00042852/

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