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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
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Volume: 66  Issue: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)
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Maneuverability,stability and controllability of aircrafts 
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.
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