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Study on shock wave and Turbulent Boundary Layer Interactions in a Square Duct at Mach 2 and 4

Journal of Thermal Science 2006年第1期15卷 37-42页

作者： Hiromu SUGIYAMA Ryojiro MINATO Kazuhide MIZOBATA Akira TOJO Yohei MUTO Department of Mechanical Systems Engineering Muroran Institute of Technology 27-1 Mizumoto Muroran Hokkaido 050-8585 Japan Graduate School Muroran Institute of Technology

In this paper, the outline of the Mach 4 supersonic wind tunnel for the investigation of the supersonic internal flows in ducts was firstly described. Secondly, the location, structure and characteristics of the Mach 2 and Mach 4 pseudo-shock waves in a square duct were investigated by color schlieren photographs and duct wall pressure fluctuation measurements. Finally, the wall shear stress distributions on the side, top and bottom walls of the square duct with the Mach 4 pseudo-shock wave were investigated qualitatively by the shear stress-sensitive liquid crystal visualization method. The side wall boundary layer separation region under the first shock is narrow near the top wall, while the side wall boundary layer separation region under the first shock is very wide near the bottom wall.

关键词： supersonic internal flow pseudo-shock wave flow visualization shear stress-sensitive liquid crystal.

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Experimental Study on shock wave Structures in Constant-area Passage of Cold Spray Nozzle

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Journal of Thermal Science 2007年第1期16卷 40-45页

作者： Hiroshi KATANODA Takeshi MATSUOKA Kazuyasu MATSUO Dept.Mechanical Engineering Kagoshima University1-21-40 KorimotoKagoshima890-0065 Japan Takagi Precision Dies Co. Ltd.2-4-1 Ishida-MinamiMinami-kuKitakyushuFukuoka802-0836 Japan Dept.Mechanical Systems and Environmental Engineering The University of Kitakyushu1-1 HibikinoWakamatsukuKitakyushuFukuoka808-0135 Japan

Cold spray is a technique to make a coating on a wide variety of mechanical or electric parts by spraying solid particles accelerated through a high-speed gas flow in a converging-diverging nozzle. In this study, pseudo-shock waves in a modeled cold spray nozzle as well as high-speed gas jets are visualized by schlieren technique. The schlieren photographs reveals the supersonic flow with shock train in the nozzle. Static pressure along the barrel wall is also measured. The location of the head of pseudo-shock wave and its pressure distribution along the nozzle wall are analytically explained by using a formula of pseudo-shock wave. The analytical results show that the supersonic flow accompanying shock wave in the nozzle should be treated as pseudo-shock wave instead of normal shock wave.

关键词： Supersonic Flow pseudo-shock wave Jet Flow Cold Spray

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