Art

J-GLOBAL ID：200902252960713304   Reference number：07A0452355

Investigation of Three-Dimensional Normal Shock-Wave/Boundary-Layer Interaction in a Transonic Diffuser Flow

遷音速ディフューザ内における垂直衝撃波/境界層干渉流れの三次元構造解析

Author (4)： ONO DAISUKE (九大) ,  HANDA TARO (九大) ,  AOKI TOSHIYUKI (九大) ,  MASUDA MITSUHARU (九大)
Material： 日本機械学会論文集 B編  (Transactions of the Japan Society of Mechanical Engineers. Series B)
Volume： 73  Issue： 728  Page： 1002-1007  Publication year： Apr. 25, 2007 
JST Material Number： F0036B  ISSN： 0387-5016  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： *transonic flow ,...

   To see more with JDream III (charged).   {{ this.onShowAbsJLink("http://jdream3.com/lp/jglobal/index.html?docNo=07A0452355&from=J-GLOBAL&jstjournalNo=F0036B") }}

JST classification (1)： High-speed aerodynamics  (BC03000C)

Reference (13)：

• CHRISS, R. M. An LDA Investigation of the Normal Shock Wave Boundary Layer Interaction. La Recherche Aerospatiale. 1990, 1990-2, 1-15
• HANDA, T. Three-dimensional Normal Shock-Wave/Boundary-Layer Interaction in a Rectangular Duct. AIAA Journal. 2005, 43, 10, 2182-2187
• DOEFFER, P. Reynolds Number Effect on Separation Structures at Normal Shock Wave/Turbulent Boundary-Layer Interaction. AIAA Journal. 1989, 27, 9, 1206-1212
• BEJM, M. An Effect of Test Section Span on the Shock Wave-Turbulent Boundary-Layer Interaction. 4th Int. Symp. on Experimental and Computational Aerothermodynamics of Internal Flows, 1999. 1999, 1, 102-110
• GEROLYMOS, G. A. Computation of Unsteady Three-Dimensional Transonic Nozzle Flows using k-ε Turbulence Closure. AIAA Journal. 1996, 34, 7, 1331-1340

Terms in the title (6)： ディフューザ ,  垂直衝撃波 ,  境界層 ,  干渉 ,  流れ ,  構造解析