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有翼宇宙往還機型全機模型の逆対称モードフラッタ
https://jaxa.repo.nii.ac.jp/records/40184
https://jaxa.repo.nii.ac.jp/records/401844104a0e5-5c0d-4fb4-aafc-d031b435a822
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr0001342.pdf (758.2 kB)
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|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 有翼宇宙往還機型全機模型の逆対称モードフラッタ | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2ロケット打上げ型有翼回収機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | チップフィン形態翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非平面翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ解析 | |||||
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 | 振動特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 模型支持装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空気力 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 orbiting plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tip fin wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | non planar wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter analysis | |||||
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 | vibration characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | model supporting equipment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamic force | |||||
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 | Anti-symmetric mode flutter of winged reentry space vehicle | |||||
著者 |
神田, 淳
× 神田, 淳× 上田, 哲彦× Kanda, Atsushi× Ueda, Tetsuhiko |
|||||
著者所属 | ||||||
航空宇宙技術研究所 機体部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 機体部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Airframe Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Airframe Division | ||||||
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 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory 巻 1342, p. 1-25, 発行日 1997-12 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 日本で開発が進められている有翼宇宙往還機HOPE(H-2ロケット打上げ型有翼回収機)はチップフィン形態の非平面翼を有している。この全機模型を製作しロール自由度制御機構を有する特殊支持装置を組み合せ、航空宇宙技術研究所の遷音速風洞で逆対称モードフラッタ実験を行った。実験からいくつかのフラッタポイントが得られ、DPM(Doublet-Point Method)による非定常空気力を用いてフラッタ解析の結果と比較したところ、亜音速において良く一致し、超音速領域については音速を超えた領域でフラッタ速度が急に増加する結果が得られ、解析値は大きく安全側となった。マッハ数がさらに大きくなると両者はまた一致する傾向を示した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The reentry winged space vehicle 'HOPE (H-2 Orbiting Plane)' project is proceeding. HOPE has a tip-fin wing which forms a non-planar wing. Anti-symmetric mode flutter experiments were conducted on a similar configuration model to HOPE by using the sting supporting system in which the rolling mode can be controlled in a transonic wind tunnel (NAL). Several flutter points have been obtained for a single model. The results of the experiments and those of the analysis by DPM (Doublet-Point Method) are compared. The comparison shows good agreement in the subsonic region. In the supersonic region, however, the experimental flutter speed rises considerably, making the analytical results conservative. It has a tendency to agree again as the Mach number increases. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001441000 | |||||
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 TR-1342 |