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突起を用いた起動停止荷重低減法の検討について
https://jaxa.repo.nii.ac.jp/records/3823
https://jaxa.repo.nii.ac.jp/records/3823df9d70d4-c82c-425a-95cb-87e23ed2e5b5
名前 / ファイル | ライセンス | アクション |
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AA1530024004.pdf (1.0 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-04-28 | |||||
タイトル | ||||||
タイトル | 突起を用いた起動停止荷重低減法の検討について | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Investigation of starting loads reduction technique using a protuberance | |||||
著者 |
飯島, 秀俊
× 飯島, 秀俊× 永井, 伸治× 西島, 寛典× 木村, 毅× Iijima, Hidetoshi× Nagai, Shinji× Nishijima, Hironori× Kimura, Takeshi |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
株式会社IHIエアロスペース・エンジニアリング(ISE) | ||||||
著者所属 | ||||||
株式会社IHIエアロスペース・エンジニアリング(ISE) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Engineering Co. Ltd. (ISE) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Engineering Co. Ltd. (ISE) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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86-第90回風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 86th-90th meeting 巻 JAXA-SP-14-011, p. 21-25, 発行日 2015-03-25 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第87回風洞研究会議 (2011年11月17日-18日) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Wind Tunnel Technology Association 87th Meeting (November 17-18, 2011) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Starting loads reduction technique using a protuberance was investigated in the JAXA 1m by 1m supersonic wind tunnel. A protuberance was set upstream from the model on the upper and lower nozzle wall. As a result, it was found that the shock wave by the protuberance induced a decelerated area around the model and reduced more than 20% of the starting load of normal force at a Mach number of 3.0. This deceleration by the shock wave from the protuberance was confirmed by pressure of the model surface. Furthermore, shock wave strength passing through the model was weakened in this decelerated area. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
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: AA1530024004 | |||||
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-14-011 |