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円錐ポートテイル・円錐フレヤーの圧力係数抗力係数に対する気体の不完全性の影響その1
https://jaxa.repo.nii.ac.jp/records/44108
https://jaxa.repo.nii.ac.jp/records/44108edf5bf12-1ae7-4498-a1b6-6437204adea2
名前 / ファイル | ライセンス | アクション |
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naltm00525.pdf (949.6 kB)
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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 | 円錐ポートテイル・円錐フレヤーの圧力係数抗力係数に対する気体の不完全性の影響その1 | |||||
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 | Theoretical investigation of real gas effects on Flare and Boattails | |||||
著者 |
野溝, 国生
× 野溝, 国生× NOMIZO, Kunio |
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著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
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 525, p. 17, 発行日 1983-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | IN this report, the difference of the pressure coefficient and the drag coefficient between ideal gas and real gas was investigated on flare and boattasls at supersonic speed. For this porpose, the characteristics method was employed. And the difference of the drag coefficient, and the pressure coefficient between ideal gas and real gas was investigated. Also, the difference of the drag coefficient between real gas and the boundary layer was investigated. It has been found that in some region of high density and low temperature, the drag coefficient of real gas is comparable to that of the boundary layer. | |||||
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: NALTM0525000 | |||||
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-525 |