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Experimental and Three—Dimensional Numerical Study on Under—Expanded Impinging Jets
引用本文:MinoruYaga KenshiUeda 等. Experimental and Three—Dimensional Numerical Study on Under—Expanded Impinging Jets[J]. 热科学学报(英文版), 2000, 9(4): 316-321. DOI: 10.1007/s11630-000-0070-6
作者姓名:MinoruYaga KenshiUeda 等
作者单位:Department of Mechanical Systems Engineering,Faculty of Engineering,University of the Ryukyus Senbaru 1,Okinawa,903-0213,JAPAN
摘    要:IntroductionUnder-expanded impinging jets have attracted theinterest of many researchers not only because they havepotentially engineering applications such as surfacecooling devicesl'], and plasma spray coating['], alsobecause they are not fully understood yet[' 5]. Goldsteinet al. confirmed that the stagnation temperature near thestagnation region on the impinging plate is larger thanthat in the settling chamber despite no heat added to theflow during its process from the settling chamber to…

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Experimental and three-dimensional numerical study on under-expanded impinging jets
Minoru Yaga,Kenshi Ueda,Tomohiro Ohshiro,Izuru Senaha,Kenyu Oyakawa. Experimental and three-dimensional numerical study on under-expanded impinging jets[J]. Journal of Thermal Science, 2000, 9(4): 316-321. DOI: 10.1007/s11630-000-0070-6
Authors:Minoru Yaga  Kenshi Ueda  Tomohiro Ohshiro  Izuru Senaha  Kenyu Oyakawa
Affiliation:(1) Department of Mechanical Systems Engineering, Faculty of Engineering, University of the Ryukyus, Senbaru 1, 903-0213 Okinawa, Japan
Abstract:In this paper, under-expanded impinging jets issued from converging circular and rectangular nozzles were investigated. The ratio of the distance between the nozzle exit and the plate L to the diameter D was set at 2, 3, 4 for the circular nozzle and 2, 3 for the rectangular nozzle. Two-dimensional temperature and static pressure distributions on the impinging plate were measured using an infrared camera and a semi-conductor pressure sensor and flow fields were visualized by means of schlieren method. Three-dimensional numerical calculations were also conducted by solving the three-dimensional compressible Euler equations and compared to the experimental results. As a result, it is found that the numerical calculations for the circular and the rectangular nozzles are in good agreement with the experiments. In the experiments, it is found that the stagnation temperature on the plate depends on the pressure in the settling chamber and the distance between the nozzle exit and the plate. The temperature and pressure distributions in the experiments illustrate that even in the case of the circular nozzle, the distributions on the impinging plate are non-axisymmetric, which is confirmed by the three dimensional calculations. The calculation for the rectangular nozzle indicates that two circulating regions occur immediately upstream of the plate.
Keywords:compressible flow   shock wave   under-expanded impinging jet   CFD   surface temperature.
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