Ishikawajima-Harima Heavy Industries Co Ltd
Ishikawajima-Harima Heavy Industries Co Ltd
Ishikawajima-Harima Heavy Industries Co Ltd
Ishikawajima-Harima Heavy Industries Co Ltd
Science University of Tokyo
National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory
巻
30
ページ
65 - 68
発行年
1996-01
会議概要（会議名, 開催地, 会期, 主催者等）
航空宇宙技術研究所 7-9 Jun. 1995 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan
There are lots of the mixing flows on the hypersupersonic transport propulsion system. For instance, the mixing between the exhaust jet and the entrained flow in the mixer-ejector nozzle to reduce the noise level at the take off and the mixing between the ram air and the turbo air in the front mixing component operating for the dual mode of the the hypersupersonic transport propulsion system. In the research and the development of this system it is very useful for predicting the mixing characteristics to design components and improve the performance of this system. In this paper the comparison between the analysis results and the test results of above two kinds flows are reported.
超音速機用推進システムにおける混合流解析
nalsp0030012.pdf
(285.15KB)
