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Numerical Simulation of Two-Dimensional Freejet Flow-Fields
https://jaxa.repo.nii.ac.jp/records/31275
https://jaxa.repo.nii.ac.jp/records/31275425794f1-1b92-4abc-ac53-fd618d06b732
名前 / ファイル | ライセンス | アクション |
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SA0033536.pdf (370.4 kB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Numerical Simulation of Two-Dimensional Freejet Flow-Fields | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
著者 |
TESHIMA, Koji
× TESHIMA, Koji× NAKATSUJI, Hiroyuki |
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著者所属(英) | ||||||
en | ||||||
Department of Aeronautical Engineering, Kyoto University. | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aeronautical Engineering, Kyoto University. | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science | |||||
書誌情報 |
en : The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Symposium on Mechanics for Space Flight 1985 巻 4, p. 89-95, 発行日 1986-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Supersonic jet flow-fields from a two-dimensional sonic nozzle are computed using the piecewise linear method. The sonic radius for a two-dimensional source flow is estimated using the numerical results. It is shown that the flow properties on the jet axis can be approximated by the two-dimensional source flow at large distances from the nozzle. The distance of the normal shock from the nozzle increases with the stagnation to ambient pressure ratio, but is somewhat larger than experiments. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0288-433X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA10455137 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0033536000 |