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計測局所マッハ数による非平面翼のフラッタ限界値補正
https://jaxa.repo.nii.ac.jp/records/6527
https://jaxa.repo.nii.ac.jp/records/6527e41046c3-330a-44ae-ab15-b35966bb6fa7
名前 / ファイル | ライセンス | アクション |
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48061002.pdf (1.4 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 | 計測局所マッハ数による非平面翼のフラッタ限界値補正 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | DPM | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ境界 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低超音速領域 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再突入機 | |||||
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 | 圧力測定 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DPM | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter boundary | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low supersonic region | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry vehicle | |||||
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 | pressure measurement | |||||
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 | Correction of flutter boundary of non-planar wing using measured local Mach number | |||||
著者 |
神田, 淳
× 神田, 淳× 甲斐, 高志× 中村, 俊哉× Kanda, Atsushi× Kai, Takashi× Nakamura, Toshiya |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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69回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 69th Meeting 巻 JAXA-SP-04-008, p. 8-12, 発行日 2005-02-28 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | For the anti-symmetric flutter speeds of a tip-fin-shaped reentry space vehicle model, numerical predictions using Doublet-Point Method (DPM) have been different from experimental results in a part of lower supersonic region. The cause of the discrepancy is suspected to be that the local flow over the wing differs from the free stream. Instead of free stream Mach numbers, measured local Mach numbers are adopted for flutter boundary analyses, and the corrected numerical results show good agreement with experimental ones. Therefore, it is made clear that the correction by local Mach numbers improves the accuracy of the flutter boundary. | |||||
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: AA0048061002 | |||||
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-04-008 |