WEKO3
アイテム
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遷音速動安定試験装置の開発
https://jaxa.repo.nii.ac.jp/records/2399
https://jaxa.repo.nii.ac.jp/records/2399d7d5cf0f-f211-4181-bf35-0acd74e21997
名前 / ファイル | ライセンス | アクション |
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47413000.pdf (5.6 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 | 遷音速動安定試験装置の開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 強制振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 慣性モーメント | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | データ取得システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的標準模型 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | forced vibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | moment of inertia | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | data acquisition system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | standard dynamics model | |||||
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 | Development of dynamic stability equipment for transonic wind tunnel | |||||
著者 |
三輪, 等
× 三輪, 等× 上野, 真× Miwa, Hitoshi× Ueno, Makoto |
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著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Foundation for Promotion of Japanese Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-03-021, 発行日 2004-03-25 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | To measure dynamic stability parameters of HOPE-X at the NAL 2 m Transonic Wind Tunnel, new type of forced oscillation pitch/yaw and roll apparatus was developed. The cams applied in the drive apparatus are relatively short longitudinally so as to cope with high load and high drive frequency when used in the transonic region. Also developed were new balances with beams of high stiffness for pitch/yaw and roll drive apparatus. Data acquisition system for accurate dynamic measurement and parameter identification software for dynamic stability properties are used to identify very small damping parameters. To validate new apparatus and identification procedure of damping parameters a series of wind tunnel tests were carried out with a standard dynamics model (SDM). Test results at NAL 2 m Transonic Wind Tunnel showed to closely agree with those by the standard dynamics model in other facilities. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047413000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-03-021 |