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Characteristics of Compression Wave Caused by Reflection of Expansion Wave at Open End of Tube
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作者 tsuyoshiyasunobu ShigeruKuchii +1 位作者 HideoKashimura ToshiakiSetoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2002年第2期97-103,共7页
When an expansion wave propagated along a constant area straight tube reaches at the open end, the negative impulsive wave and the compression wave are formed by the emission and reflection of expansion wave. The nega... When an expansion wave propagated along a constant area straight tube reaches at the open end, the negative impulsive wave and the compression wave are formed by the emission and reflection of expansion wave. The negative impulsive wave is emitted toward the surrounding area and causes an impulsive noise like the sonic boom. The compression wave propagates in the tube toward the upstream and may cause the impulsive noise at the surrounding area of tube portal. With the advance of industrial engineering, it seems that the discharging of the expansion wave will become important problems. In this study, the experimental and numerical investigations are carried out using the shock tube and the TVD numerical method. The formation process of compression wave near the open end, the relationship with the compression wave and the expansion wave and the characteristics of compression wave are discussed. 展开更多
关键词 COMPRESSIBLE FLOW UNSTEADY FLOW compression WAVE EXPANSION WAVE numerical analysis.
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Temperature Distribution on Inclined Plate Caused by Interaction withSupersonic Jet
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作者 tsuyoshiyasunobu ToshiakiSetoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2000年第4期339-344,共6页
The Phenomena of the interaction between a supersonic jet and an obstacle is a very interesting and important problem relating to the industrial engineering. This paper aims to investigate the characteristics of the t... The Phenomena of the interaction between a supersonic jet and an obstacle is a very interesting and important problem relating to the industrial engineering. This paper aims to investigate the characteristics of the two-dimensional temperature distribution on an inclined plate surface and the relation between the temperature distribution and some shock waves formed in the flow field. In this study, the measurement of temperature distribution on an inclined plate surface and the now visualization has carried out for various conditions using the thermo-sensitive liquid crystal sheet and the schlieren method. The two dimensional temperature distribution on the plate surface is clearly obtained by the thermo-sensitive liquid crystal sheet. The relation between the temperature distribution on an inclined plate surface and some shock waves reached at a plate surface is discussed. In this paper, the characteristics of the temperature distribution and the maximum temperature, and some other experimental evidences are presented. 展开更多
关键词 compressible flow supersonic jet Mach disk barrel shock.
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