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カプセル型回収体の極超音速三分力測定試験
https://jaxa.repo.nii.ac.jp/records/44059
https://jaxa.repo.nii.ac.jp/records/44059e7a4c6db-f26c-46c0-ab89-bfe44b9b1734
名前 / ファイル | ライセンス | アクション |
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naltm00476.pdf (2.4 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 | カプセル型回収体の極超音速三分力測定試験 | |||||
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 Static Stability of Capsule-Type Re-Entry Bodies | |||||
著者 |
山本, 行光
× 山本, 行光× 渡辺, 光則× 野村, 茂昭× 穂積, 弘一× 小山, 忠勇× YAMAMOTO, Yukimitsu× WATANABE, Mitsunori× NOMURA, Shigeaki× HOZUMI, Koichi× KOYAMA, Tadao |
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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 | ||||||
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 476, p. 53, 発行日 1982-10 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hypersonic wind tunnel tests were made to determine the aerodynamic characteristics of some capsule type re-entry bodies at Mach number 7.1 and at angles of attack from 0°to 20°.The Reynolds number based on maximum body diameter varied from 4.5 × 105 to 18×105.Tests were made to determine the appropriate nose and shoulder radii of these capsules necessary to obtain optimum configurations for the aerodynamic requirements.The nose radius R1 is changed from 2 to 4 and shoulder radius R2 from 0 to 0.1,which are nondimensionalized by the maximum radius R3 of the sharp shoulder capsules,respectively.Results of the tests indicate that higher lift to drag ratio L/D and lower trim angles δ can be obtained by increasing the nose radius.The same trends are shown when decreasing the shoulder radius.The Reynolds number shows a slight effect on the lift and drag coefficients CL,CD,but no remarkable differences can be seen in other aerodynamic coefficients. | |||||
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: NALTM0476000 | |||||
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-476 |