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カプセル型回収体極超音速動安定特性試験
https://jaxa.repo.nii.ac.jp/records/44139
https://jaxa.repo.nii.ac.jp/records/441394664215e-93cf-4e9e-880f-855ae1bc79ac
名前 / ファイル | ライセンス | アクション |
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naltm00556.pdf (1.7 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 | カプセル型回収体極超音速動安定特性試験 | |||||
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_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 | Measurements of Dynamic Stability of Capsule-Type Re-Entry Vehicles at Hypersonic Speeds | |||||
著者 |
山本, 行光
× 山本, 行光× 渡辺, 光則× 野村, 茂昭× 小山, 忠勇× 穂積, 弘一× 吉沢, 昭× 伊藤, 哲一× 高塚, 均× YAMAMOTO, Yukimitsu× WATANABE, Mitsunori× NOMURA, Shigeaki× KOYAMA, Tadao× HOZUMI, Koichi× YOSHIZAWA, Akira× ITO, Tetsuichi× TAKATSUKA, HITOSHI |
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著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
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資料 en : Technical Memorandum of National Aerospace Laboratory 巻 556, p. 19, 発行日 1986-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hypersonic wind tunnel tests were conducted to measure the pitch damping characteristics of a series of capsule-type vehicles at a Mach number of 7. 1. Data were obtained utilizing thesmall amplitude free oscillation technique at angles of attack from 0 to 10deg at a Reynolds number of 4.5×104, based on a unit length (cm). Model configurations are classified into two types, i. e. , 1) a blunt cone type (S-type) which consists of a model with half cone angles of 6゜ and 10゜, and 2) acapsule type (M-type) which has a blunted forebody followed by a conical boattail and cylinder. Results of the tests indicate that S-type models are dynamically stable through the angles of attack, whereas M-type models reveal dynamic instability at low angles of attack. These trends are thought to be due to flow reattachment effects occurring on the cylinder surface of the capsules. These undamping results can be eliminated or greatly reduced by taking angles of attack. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0556000 | |||||
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 TM-556 |