@techreport{oai:jaxa.repo.nii.ac.jp:00044590,
 author = {遠藤, 浩 and 中谷, 輝臣 and 飛田和, 茂 and 桑野, 尚明 and 戸田, 亘洋 and ENDO, Hiroshi and NAKAYA, Teruomi and HIDAWA, Shigeru and KUWANO, Naoaki and TODA, Nobuhiro},
 month = {Oct},
 note = {A semi-empirical method is presented in this paper to calculate the path and the induced velocity of a round turbulent jet exhausting into a uniform cross flow. By analogy with a suction cylinder and based on a vortex-sheet theory developed in the previous paper, the jet is replaced by a vortex-doublet which is an idealized representation of the trailing vortex-sheet on the surface of the jet, the induced velocity around the jet being assumed as induced by the vortex-doublet. The comparison of calculated downwash and sidewash angles of the induced flow with experimental results obtained in 6M low-speed wind tunnel of NAL, it is proved that the present method can be used as a working basis for investigating the interaction with the airframe of a jet-lift VTOL aircraft through the far induced field of exhaust gas., 資料番号: NALTR0343000, レポート番号: NAL TR-343},
 title = {一様流中に大きな角度で吹き出したジェットの径路と誘導速度場},
 year = {1973}
}