屈曲2重円錐の超音速風洞試験

Material type: 文書・図像類

Author: 関根, 英夫ほか

Publisher: 航空宇宙技術研究所

Publication date: 1993-05

Material Format: Digital

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Note (General)：: AOTV(空力制動型軌道間輸送機)の1形態である屈曲2重円錐の超音速風洞実験結果を示す。超高速飛行体についても低超音速域空力性能試験の必要が考えられる。本試験は特に大迎角試験、表面の流れの剥離測定、底面圧計測および簡単な理論推定法のチェックなどに重点がおかれた。Preliminary wind tu...

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Material Type: 文書・図像類
Title: 屈曲2重円錐の超音速風洞試験
Author/Editor: 関根, 英夫
野田, 順一
石田, 清道
谷, 喬
Sekine, Hideo
Noda, Junichi
Ishida, Kiyomichi
Tani, Takashi
Author Heading: 関根, 英夫
野田, 順一
石田, 清道
谷, 喬
Sekine, Hideo
Noda, Junichi
Ishida, Kiyomichi
Tani, Takashi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1993-05
Publication Date (W3CDTF): 1993-05
Alternative Title: Investigation of experimental bent-nose biconic design in supersonic flow
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory
No. or year of volume/issue: 1205
Volume: 1205
Pages: 1-20
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Subject Heading: 超音速空気力学
超音速流れ
超音速風洞
鼻曲り2重円錐
AOTV
空力制動型軌道間輸送機
宇宙飛行体
大迎角試験
圧力分布計測
オイルフロー試験
底面圧計測
凹面底面圧
平面底面圧
ニュートン流近似
supersonic aerodynamics
supersonic flow
supersonic wind tunnel
bent nose biconic
Aeroassisted Orbital Transfer Vehicle
space vehicle
large angle of attack test
pressure distribution measurement
oil flow test
base pressure measurement
concave base base pressure
flat base base pressure
Newtonian flow approximation
Target Audience: 一般
Note (General): AOTV(空力制動型軌道間輸送機)の1形態である屈曲2重円錐の超音速風洞実験結果を示す。超高速飛行体についても低超音速域空力性能試験の必要が考えられる。本試験は特に大迎角試験、表面の流れの剥離測定、底面圧計測および簡単な理論推定法のチェックなどに重点がおかれた。
Preliminary wind tunnel tests of a Bent-Nose Biconic were conducted in the NAL 1m X 1m blow-down supersonic wind tunnel to evaluate its aerodynamics in the moderate supersonic range. Aerodynamic data at attack angles of up to 50 deg was obtained for a 30 deg bent-sting. A flow-separated zone on the rear side of the body was observed by surface pressure distribution and oil-flow tests. Estimates based on Newtonian flow theory were not accurate when the attack angle was small for this rather slender configuration.
資料番号: AA0004220000
レポート番号: NAL TR-1205
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