@inproceedings{oai:jaxa.repo.nii.ac.jp:00037188,
 author = {重見, 仁 and 神田, 宏 and 佐藤, 衛 and 須谷, 記和 and Shigemi, Masashi and Kanda, Hiroshi and Sato, Mamoru and Sudani, Norikazu},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Jan},
 note = {22-23 May 1997 (58th). 27-28 Nov. 1997 (59th), 22-23 May 1997 (58th). 27-28 Nov. 1997 (59th), 航空宇宙技術研究所2次元風洞は1979年に竣工し、実機相当のレイノルズ数を実現できる風洞として、多くの試験に用いられてきた。しかし近年老朽化が進み試験の実施に支障を来すことが多くなった。そこで1995年度から改修に取り掛かり、近く完成する見通しである。新しい2次元風洞では老朽化に対する処置に加えて、測定部の大きさの変更、可変ノズルの導入などを盛り込み、可能な試験の範囲を拡張すると同時に、作業性の向上、データの高精度化を図った。本報告は新しい2次元風洞の概要について述べる。, The NAL transonic two-dimensional wind tunnel was constructed in 1979, and has been used as a facility, in which tests can be realized under the condition of Reynolds number equivalent to that of an aircraft. However, it became so superannuated recently as difficult to carry out tests without trouble. Hence revitalization of the facility was started in 1995, and it will be completed at an early date. For the renewed two-dimensional wind tunnel, the improvement of operational function and data accuracy were attempted, simultaneously with expanding the possible test range by incorporating such renewal as making measuring part large-scaled and introducing a variable nozzle, in addition to the treatment for superannuating. This paper outlines the renewed two-dimensional wind tunnel., 資料番号: AA0001434006, レポート番号: NAL SP-38},
 pages = {57--66},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {航技研二次元風洞の改修},
 volume = {38},
 year = {1998}
}