@techreport{oai:jaxa.repo.nii.ac.jp:00044237,
 author = {半澤, 麻雄 and 小國, 保男 and 鈴木, 正光 and 唐澤, 敏夫 and 小松, 行夫 and 安藤, 泰勝 and HANZAWA, Asao and OGUNI, Yasuo and KARASAWA, Toshio and KOMATSUNAL, Yukio and ANDOJAST, Yasukatsu},
 month = {Jan},
 note = {航空宇宙技術研究所2m×2m遷音速風洞の第3カート上にフラッタ緊急停止装置が1993年度に設置された。この装置を用いた風洞試験の結果，全開時のマッハ数低下量については計画通りであるが，圧力変動を生ずることが分った。今回，この不具合を解消する改良をフラッタ停止板と開度について行い，良い結果が得られたので，改良の内容と試験結果について報告する。, A flutter emergency stopper was installed on the III cart device of the 2m×2m transonic wind tunnel at the National Aerospace Laboratory in 1993. Wind tunnel testing with the device revealed that while the decline in Mach number obtained when  the flutter stopper opens coincided with the design value, pressure fluctuation did occur. To eliminate this pressure fluctuation, improvements were made to the flutter stopper plate and opening angle . Subsequent test results confirmed the effectiveness and safety of the flutter-suppressing device. This report presents the improvements made to the flutter-suppressing device, the tests conducted and test results., 資料番号: NALTM0767000, レポート番号: NAL TM-767},
 title = {遷音速風洞フラッタ緊急停止装置性能試験(その2)　第3カート用装置},
 year = {2002}
}