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スパイク付き飛しょう体の空力特性制御に関する実験研究
http://hdl.handle.net/10258/00010355
http://hdl.handle.net/10258/00010355810a0c56-752e-451d-982e-18654cf9befc
名前 / ファイル | ライセンス | アクション |
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JJSASS_55_644_418_425 (731.5 kB)
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Item type | 学術雑誌論文 / Journal Article.(1) | |||||||||||
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公開日 | 2021-03-03 | |||||||||||
タイトル | ||||||||||||
言語 | ja | |||||||||||
タイトル | スパイク付き飛しょう体の空力特性制御に関する実験研究 | |||||||||||
言語 | ||||||||||||
言語 | jpn | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Aerodynamic characteristics | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Compressible Flows | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Aerospikes | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Separation | |||||||||||
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 | journal article | |||||||||||
アクセス権 | ||||||||||||
アクセス権 | open access | |||||||||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||||||||
著者 |
小林, 弘明
× 小林, 弘明× 吹場, 活佳× 本郷, 素行× 佐藤, 哲也× 溝端, 一秀
WEKO
801
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室蘭工業大学研究者データベースへのリンク | ||||||||||||
溝端 一秀(MIZOBATA Kazuhide) | ||||||||||||
http://rdsoran.muroran-it.ac.jp/html/100000207_ja.html | ||||||||||||
抄録 | ||||||||||||
内容記述タイプ | Abstract | |||||||||||
内容記述 | Experimental studies on telescopic aerospikes for aerodynamic control are reported in this paper. Parametric study on the aerodynamic characteristics of the aerospike has performed including the effect of spike length L, base diameter of tip cone D, spike translating speed and direction. The Axial force coefficient Ca of the aerospike suddenly increases at L/D=3.0 due to flow mode transition from the separation to the reattachment. Reattachment/separation flow mode transition phenomenon can be applicable to a newly invented aerodynamic control device, which is called air-breathing aerospike. In this paper, verification test results of this air-breathing aerospike are also reported. A small solenoid valve in the body cylinder successfully controls reattachment/separation flow mode transition at the angle of attacks from 0 to 12 degree. The spiked bodies’ Ca varies according to the mode transition. As a result, we can control the aerodynamic property of the spiked body by opening/closing the valves periodically. | |||||||||||
言語 | en | |||||||||||
書誌情報 |
ja : 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences 巻 55, 号 644, p. 418-425, 発行日 2007-09-05 |
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出版者 | ||||||||||||
言語 | ja | |||||||||||
出版者 | 日本航空宇宙学会 | |||||||||||
出版者版へのリンク | ||||||||||||
10.2322/jjsass.55.418 | ||||||||||||
https://doi.org/10.2322/jjsass.55.418 | ||||||||||||
DOI | ||||||||||||
関連タイプ | isIdenticalTo | |||||||||||
識別子タイプ | DOI | |||||||||||
関連識別子 | 10.2322/jjsass.55.418 | |||||||||||
日本十進分類法 | ||||||||||||
主題Scheme | NDC | |||||||||||
主題 | 538 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | PISSN | |||||||||||
収録物識別子 | 13446460 | |||||||||||
権利 | ||||||||||||
言語 | ja | |||||||||||
権利情報 | © 2007 日本航空宇宙学会 | |||||||||||
著者版フラグ | ||||||||||||
出版タイプ | VoR | |||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||
フォーマット | ||||||||||||
内容記述タイプ | Other | |||||||||||
内容記述 | application/pdf |