@techreport{oai:jaxa.repo.nii.ac.jp:00045048,
 author = {犬丸, 矩夫 and 高橋, 侔 and 広末, 健一 and 戸田, 亘洋 and 桑野, 尚明 and INUMARU, Norio and TAKAHASHI, Hitoshi and HIROSUE, Kenichi and TODA, Nobuhiro and KUWANO, Naoaki},
 month = {Nov},
 note = {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},
 title = {ファンジェットSTOL機の空力特性},
 year = {1983}
}