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振動同定除去法による衝撃風洞計測データからの空力6分力の推定
https://jaxa.repo.nii.ac.jp/records/6431
https://jaxa.repo.nii.ac.jp/records/6431af76df1a-539f-414c-89c9-75d5d0c945b2
名前 / ファイル | ライセンス | アクション |
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48471007.pdf (1.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 振動同定除去法による衝撃風洞計測データからの空力6分力の推定 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速風洞 | |||||
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 | 風洞模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動同定除去法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動測定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞天秤 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic shock 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 | wind tunnel model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic force | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel apparatus | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | oscillation identification technique | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration measurement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel balance | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Aerodynamic force extraction from hypersonic shock tunnel measurement using the oscillation identification technique | |||||
著者 |
渡利, 實
× 渡利, 實× Watari, Minoru |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 風洞技術開発センター | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Wind Tunnel Technology Center, 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特別資料: 第73回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 73rd Meeting 巻 JAXA-SP-04-014, p. 50-53, 発行日 2005-03-30 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In a hypersonic shock tunnel, it is essential to extract aerodynamic force from oscillation-contaminated measurement. This paper proposes an oscillation identification technique method. The method identifies aerodynamic force by the parameter-matching technique. Verification test, applying this method to HB2 standard model, was satisfactory with completely consistent results. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0048471007 | |||||
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-SP-04-014 |