Art

J-GLOBAL ID：201202227136004990   Reference number：12A0717626

Experimental study of interaction between supersonic duct flow and jets surrounded by the porous cavity

超音速ダクト流と多孔質キャビティで囲まれた噴流間の相互作用に関する実験的研究

Author (5)： KUNIYOSHI Nao (Dep. of Mechanical Systems, Facility of Engineering, Univ. of the Ryukyus, 1 Senbaru, Nishihara, Okinawa 903-0213, JPN) ,  YAGA Minoru (Dep. of Mechanical Systems, Facility of Engineering, Univ. of the Ryukyus, 1 Senbaru, Nishihara, Okinawa 903-0213, JPN) ,  KODA Akito (Dep. of Mechanical Systems, Facility of Engineering, Univ. of the Ryukyus, 1 Senbaru, Nishihara, Okinawa 903-0213, JPN) ,  TERUYA Isao (Dep. of Mechanical Systems, Facility of Engineering, Univ. of the Ryukyus, 1 Senbaru, Nishihara, Okinawa 903-0213, JPN) ,  ISHIKAWA Masaaki (Dep. of Mechanical Systems, Facility of Engineering, Univ. of the Ryukyus, 1 Senbaru, Nishihara, Okinawa 903-0213, JPN)
Material： Experimental Thermal and Fluid Science  (Exp Therm Fluid Sci)
Volume： 40  Page： 185-194  Publication year： Jul. 2012 
JST Material Number： T0618A  ISSN： 0894-1777  Document type： Article
Article type： 原著論文  Country of issue： United States (USA)  Language： ENGLISH (EN)

Thesaurus term： *shock wave ,  *compressible flow ,  *porous medium ,  *cavity ,  *supersonic flow ,  *duct flow ,  *jet(flow) ,  *flow field ,  flow ,  detached shock wave ,  *control system ,  interaction ,  experimental equipment ,  measurement data ,  flow distribution ,  pressure distribution ,  static pressure ,  schlieren method ,  flow visualization ,  flow structure
Semi thesaurus term： flow direction

JST classification (2)： High-speed aerodynamics  (BC03000C) ,  Gas turbines  (PB02040Y)

Terms in the title (7)： 超音速 ,  ダクト流 ,  多孔質 ,  キャビティ ,  噴流 ,  相互作用 ,  実験的研究