Art

J-GLOBAL ID：201802251815520884   Reference number：18A0377071

Characteristics of Subsonic FTV Nozzle and Its Flight Demonstration

亜音速FTVノズルの特性とその飛行実証

Author (5)： HIROTA MITSUTOMO (連絡先著者(Corresponding author):[e-mail]) ,  HIROTA MITSUTOMO (室蘭工業大学機械航空創造系学科) ,  HATANAKA KAZUAKI (Department of Aerospace Engineering, Indian Institute of Science) ,  SAITO TSUTOMU (室蘭工業大学機械航空創造系学科) ,  RAO Srisha M. V. (室蘭工業大学機械航空創造系学科)
Material： 日本航空宇宙学会論文集  (Journal of the Japan Society for Aeronautical and Space Sciences)
Volume： 66  Issue： 1  Page： 1-6(J-STAGE)  Publication year： 2018 
JST Material Number： L3565A  ISSN： 1344-6460  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： wind tunnel test ,  nozzle ,  flight test ,  membrane and film ,  flow visualization ,  transient response ,  subsonic flow ,  *fluidics ,  vector control ,  thrust control ,  *remotely piloted vehicle ,  free stream ,  deflection (direction) ,  Pitot tube ,  attitude control ,  gas turbine engine ,  machine element ,  machinery ,  fluid machinery ,  turbine
Semi thesaurus term： gas turbine ,  wind tunnel experiment ,  laser sheet ,  二次噴射

Author keywords (3)： Fluidic Thrust Vectoring (FTV) Nozzle ,  Subsonic Flow ,  Flight Test UAV

JST classification (1)： Maneuverability,stability and controllability of aircrafts  (QK02040A)

Reference (20)：

• 1) Kowal, H. J.: Advances in Thrust Vectoring and the Application of Flow-control Technology, Can. Aeronautics Space J., 48, 2 (2002), pp. 145-151.
• 2) Deere, K. A.: Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center, AIAA 2003-3800, 2003.
• 3) Federspiel, J., Bangert, L., Wing, D. J. and Hawkes, T.: Fluidic Control of Nozzle Flow-Some Performance Measurements, AIAA 95-2605, 1995.
• 4) Deere, K. A. and Berrier, B. L.: Computational Study of Fluidic Thrust Vectoring Using Separation Control in a Nozzle, AIAA 2003-3803, 2003.
• 5) Wing, D. J. and Giuliano, V. J.: Fluidic Thrust Vectoring of an Axisymmetric Exhaust Nozzle at Static Conditions, FEDSM 97-3228, 1997.

Terms in the title (2)： 飛行 ,  実証