USB方式STOL機のエンジン艤装(I) 円型合流ダクトによるエンジンマッチング特性(その1)

Material type: 文書・図像類

Author: 松木, 正勝ほか

Publisher: 航空宇宙技術研究所

Publication date: 1982-02

Material Format: Digital

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Note (General)：: Purposes of this research are to obtain design data of an engine-nacelle for a USB powered high lift system on a STOL aircraft, which is being develop...

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Material Type: 文書・図像類
Title: USB方式STOL機のエンジン艤装(I) 円型合流ダクトによるエンジンマッチング特性(その1)
Author/Editor: 松木, 正勝
鳥崎, 忠雄
近藤, 博
中山, 晋
関根, 静雄
吉田, 晃
森田, 光男
越沼, 威
松田, 幸雄
藤沢, 良昭
吉田, 公則
MATSUKI, Masakatsu
TORISAKI, Tadao
KOND0, Hiroshi
NAKAYAMA, Susumu
SEKINE, Shizuo
YOSHIDA, Akira
MORITA, Mitsuo
KOSHINUMA, Takeshi
MATSUDA, Yukio
FUJISAWA, Yoshiaki
YOSHIDA, Masanori
Author Heading: 松木, 正勝
鳥崎, 忠雄
近藤, 博
中山, 晋
関根, 静雄
吉田, 晃
森田, 光男
越沼, 威
松田, 幸雄
藤沢, 良昭
吉田, 公則
MATSUKI, Masakatsu
TORISAKI, Tadao
KOND0, Hiroshi
NAKAYAMA, Susumu
SEKINE, Shizuo
YOSHIDA, Akira
MORITA, Mitsuo
KOSHINUMA, Takeshi
MATSUDA, Yukio
FUJISAWA, Yoshiaki
YOSHIDA, Masanori
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1982-02
Publication Date (W3CDTF): 1982-02
Alternative Title: An Engine Installation for Fan Jet STOL Aircraft using USB powered High Lift System(I) Engine Matching Test for Circular Confluent Exhaust Duct
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-703
No. or year of volume/issue: 703
Volume: 703
Pages: 15-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): Purposes of this research are to obtain design data of an engine-nacelle for a USB powered high lift system on a STOL aircraft, which is being developed by the National Aerospace Laboratory. In these design data, structure and strength of the engine-nacelle and conformity between an engine and its engine-nacells are the most important problems. In order to obtain engine operational characteristics for mixing a fan and a core flow, a test was performed using a FJR 710 turbo-fan engine installed in a circular confluent exhaust duct. Test parameters of interest are the length of the mixing zone and the contraction of the mixing nozzle. As a result of this investigation, it has been proved that a power-turbine output decreases with an increase of outlet pressure of the power-turbine due to the mixing. And a clue to a design method to correct engine operational matching characteristics was found.
資料番号: NALTR0703000
レポート番号: NAL TR-703
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