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Aerodynamics and Flight Capability of a Supersonic Flight Experiment Vehicle
http://hdl.handle.net/10258/00010366
http://hdl.handle.net/10258/00010366f1f7022f-9925-42b9-a8bb-753f9139728d
名前 / ファイル | ライセンス | アクション |
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TASTJ_14_30_Pg1_Pg8 (2.2 MB)
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Item type | 学術雑誌論文 / Journal Article.(1) | |||||||||||
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公開日 | 2021-03-09 | |||||||||||
タイトル | ||||||||||||
言語 | en | |||||||||||
タイトル | Aerodynamics and Flight Capability of a Supersonic Flight Experiment Vehicle | |||||||||||
言語 | ||||||||||||
言語 | eng | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Space Transportation | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Flying Test Bed | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Flight Test | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Supersonic | |||||||||||
キーワード | ||||||||||||
言語 | en | |||||||||||
主題Scheme | Other | |||||||||||
主題 | Jet Propulsion | |||||||||||
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 |
溝端, 一秀
× 溝端, 一秀
WEKO
801
× 鈴木, 祥弘× OOISHI, Sakae× KONDOH, Satoshi× 新井, 隆景× 東野, 和幸 |
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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 | With the aims of creating and validating innovative fundamental technologies for high-speed atmospheric flights, a small scale supersonic flight experiment vehicle is designed as a flying test bed. An aerodynamic configuration is proposed for the 2nd-generation vehicle with a cranked-arrow main wing and a single Air Turbo Ramjet Gas-generator-cycle (ATR-GG) engine. Its longitudinal, lateral, and control surface aerodynamics are characterized through intensive wind-tunnel tests. They are found to be quite moderate except that the directional stability deteriorates severely at large angles of attack and side slip, and that the elevon deflections for roll control cause adverse yaw. These aerodynamic anomalies will result in a tendency of roll reversal at large angles of attack. It can be prevented to some extent by coordinated rudder deflections. In addition, necessity of transonic drag reduction is clarified through thrust margin and flight capability analyses. Probability of 5 to 20 % drag reduction in the transonic regime (Mach 0.8 to 1.2) is demonstrated by configuration modification on the basis of the area rule at Mach 1.1. | |||||||||||
言語 | en | |||||||||||
書誌情報 |
en : TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 巻 14, 号 30, 発行日 2016 |
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出版者 | ||||||||||||
言語 | en | |||||||||||
出版者 | JAPAN SOC AERONAUT SPACE SCI | |||||||||||
出版者版へのリンク | ||||||||||||
10.2322/tastj.14.Pg_1 | ||||||||||||
https://doi.org/10.2322/tastj.14.Pg_1 | ||||||||||||
DOI | ||||||||||||
関連タイプ | isIdenticalTo | |||||||||||
識別子タイプ | DOI | |||||||||||
関連識別子 | 10.2322/tastj.14.Pg_1 | |||||||||||
日本十進分類法 | ||||||||||||
主題Scheme | NDC | |||||||||||
主題 | 538 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | EISSN | |||||||||||
収録物識別子 | 1884-0485 | |||||||||||
権利 | ||||||||||||
言語 | en | |||||||||||
権利情報 | © 2016 JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | |||||||||||
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 |