サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験

Material type: 文書・図像類

Author: 外立, 政隆ほか

Publisher: 航空宇宙技術研究所

Publication date: 1977-02

Material Format: Digital

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Note (General)：: This paper describes the results of a test performed on the aerodynamic effects of a jet flow from the surface of a rocket on its tail-fin surface. In...

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Material Type: 文書・図像類
Title: サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験
Author/Editor: 外立, 政隆
清水, 福壽
HASHIDATE, Masataka
SHIMIZU, Fukuji
Author Heading: 外立, 政隆
清水, 福壽
HASHIDATE, Masataka
SHIMIZU, Fukuji
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1977-02
Publication Date (W3CDTF): 1977-02
Alternative Title: Experimental Investigation of the Effects of Side Jet on a Tail-fin of a Rocket in Supersonic Flow
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-490
No. or year of volume/issue: 490
Volume: 490
Pages: 30-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): This paper describes the results of a test performed on the aerodynamic effects of a jet flow from the surface of a rocket on its tail-fin surface. In order to investigate these effects, pressure distribution on the tail-fin, pitot-pressure distribution and velocity vector distribution at the jet-core cross section were measured in a supersonic wind tunnel. Form the measured data, it was conclude that;1.The side jet ejected in the direction producing the pitch motion induces a pair of vortices at a point downstream from the jet nozzle, while the side jet ejected in the direction producing the roll motion induces only one large scale vortex. 2.In both cases, distorition of the pressure field on the tail-fin is due to the vortex or the vortices downstream of the jet nozzle.
資料番号: NALTR0490000
レポート番号: NAL TR-490
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44743&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44743&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ