@techreport{oai:jaxa.repo.nii.ac.jp:00044960,
 author = {松木, 正勝 and 鳥崎, 忠雄 and 近藤, 博 and 中山, 晋 and 関根, 静雄 and 吉田, 晃 and 森田, 光男 and 越沼, 威 and 松田, 幸雄 and 藤沢, 良昭 and 吉田, 公則 and MATSUKI, Masakatsu and TORISAKI, Tadao and KOND0, Hiroshi and NAKAYAMA, Susumu and SEKINE, Shizuo and YOSHIDA, Akira and MORITA, Mitsuo and KOSHINUMA, Takeshi and MATSUDA, Yukio and FUJISAWA, Yoshiaki and YOSHIDA, Masanori},
 month = {Feb},
 note = {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},
 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)},
 year = {1982}
}