ファンジェットSTOL機の空力特性

Material type: 文書・図像類

Author: 犬丸, 矩夫ほか

Publisher: 航空宇宙技術研究所

Publication date: 1983-11

Material Format: Digital

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Note (General)：: Research on Fan-Jet STOL aircraft was initiated by NAL in 1975 as a wind-tunnel-based program aimed at the design study of experimental STOL aircraft....

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Material Type: 文書・図像類
Title: ファンジェットSTOL機の空力特性
Author/Editor: 犬丸, 矩夫
高橋, 侔
広末, 健一
戸田, 亘洋
桑野, 尚明
INUMARU, Norio
TAKAHASHI, Hitoshi
HIROSUE, Kenichi
TODA, Nobuhiro
KUWANO, Naoaki
Author Heading: 犬丸, 矩夫
高橋, 侔
広末, 健一
戸田, 亘洋
桑野, 尚明
INUMARU, Norio
TAKAHASHI, Hitoshi
HIROSUE, Kenichi
TODA, Nobuhiro
KUWANO, Naoaki
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1983-11
Publication Date (W3CDTF): 1983-11
Alternative Title: Aerodynamic Characteristics of Fan-Jet STOL Aircraft
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-790
No. or year of volume/issue: 790
Volume: 790
Pages: 99-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): Research on Fan-Jet STOL aircraft was initiated by NAL in 1975 as a wind-tunnel-based program aimed at the design study of experimental STOL aircraft. Aerodynamic characteristics of the Augmentor Wing type model and the Upper Surface Blowing type models are examined by a series of wind-tunnel tests. Three-component longitudinal data of each model are presented. Six-component lateral data of a USB type model are also presented with four engines operating and with one engine out. The general aerodynamic trends of Powered-Lift systems are discussed through comparison with existing data. Discussions concerning the test-techniques are also included. The research was concluded in 1979, making direct contributions to the basic design of NAL Quiet STOL Experimental Aircraft.
資料番号: NALTR0790000
レポート番号: NAL TR-790
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