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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
https://jaxa.repo.nii.ac.jp/records/44237
https://jaxa.repo.nii.ac.jp/records/4423734b190c1-4aa5-4e95-a007-443cc360e86a
名前 / ファイル | ライセンス | アクション |
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naltm0000767.pdf (1.9 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 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 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flutter suppression device; transonic wind tunnel; flutter model test. | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Performance Test of Flutter Emergency Stopper for Transonic Wind Tunnel (Part 2) The III Cart Device | |||||
著者 |
半澤, 麻雄
× 半澤, 麻雄× 小國, 保男× 鈴木, 正光× 唐澤, 敏夫× 小松, 行夫× 安藤, 泰勝× HANZAWA, Asao× OGUNI, Yasuo× KARASAWA, Toshio× KOMATSUNAL, Yukio× ANDOJAST, Yasukatsu |
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著者所属 | ||||||
航空宇宙技術研究所風洞技術開発センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所風洞技術開発センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所風洞技術開発センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所風洞技術開発センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所風洞技術開発センター | ||||||
著者所属 | ||||||
JAST | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aero Space Technology | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
独立行政法人航空宇宙技術研究所資料 巻 767, p. 18, 発行日 2002-01 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 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。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1347-460X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0767000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-767 |