双発USB半截模型風洞試験

Material type: 文書・図像類

Author: 高橋, 侔ほか

Publisher: 航空宇宙技術研究所

Publication date: 1991-12

Material Format: Digital

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Note (General)：: 航空宇宙技術研究所ではSTOL実験機「飛鳥」の研究開発と共に,STOL-CADプログラムの開発,改良を行ってきた。このCADプログラムの適用範囲を2発,3発USB機へ広げるのに必要な空力データ取得を目的として,既存の4発型USB半截模型を双発型に改修して,風洞試験を実施した。本報告は同模型形態での各...

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Material Type: 文書・図像類
Title: 双発USB半截模型風洞試験
Author/Editor: 高橋, 侔
藤枝, 郭俊
岩崎, 昭人
藤田, 敏美
斉藤, 雅樹
TAKAHASHI, Hitoshi
FUJIEDA, Hirotoshi
IWASAKI, Akihito
FUJITA, Toshimi
SAITO, Masaki
Author Heading: 高橋, 侔
藤枝, 郭俊
岩崎, 昭人
藤田, 敏美
斉藤, 雅樹
TAKAHASHI, Hitoshi
FUJIEDA, Hirotoshi
IWASAKI, Akihito
FUJITA, Toshimi
SAITO, Masaki
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1991-12
Publication Date (W3CDTF): 1991-12
Alternative Title: Wind Tunnel Investigation of a Twin-Engine Jet Transport Seme-span Model with Upper Surface Blown Jet Flap
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1134
No. or year of volume/issue: 1134
Volume: 1134
Pages: 33-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Subject Heading: upper surface blowing; wind tunnel test; STOL; semi-span model; aerodynamic characteristics
Target Audience: 一般
Note (General): 航空宇宙技術研究所ではSTOL実験機「飛鳥」の研究開発と共に,STOL-CADプログラムの開発,改良を行ってきた。このCADプログラムの適用範囲を2発,3発USB機へ広げるのに必要な空力データ取得を目的として,既存の4発型USB半截模型を双発型に改修して,風洞試験を実施した。本報告は同模型形態での各種空力要素に対する空力特性を検討した結果について述べる。
In parallel with the research and development conducted by the National Aerospace Laboratory (NAL) on the experimental aircraft ″ASKA″, a short takeoff and landing (STOL)-Computer Aided Design (CAD) program for four-engine upper surface blowing (USB) aircraft was developed and refined. To apply this CAD program to twin-and three-engine USB aircraft, aerodynamic data must be acquired for twin-engine USB aircraft. This led to the present study which modified the existing four-engine USB semi-span model into a twin-engine model and subsequently conducted low-speed wind tunnel tests. Resultant aerodynamic characteristics of the numerous aerodynamic elements included in this model are described.
資料番号: NALTR1134000
レポート番号: NAL TR-1134
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