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采场复杂流场的流体动力相似与模化问题 被引量:18
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作者 丁广骧 杨胜强 张吉禄 《中国矿业大学学报》 EI CAS CSCD 北大核心 1995年第1期47-51,共5页
本文针对几何边界复杂、流态分布复杂和重力作用与机械压力p相当的复杂采场流场,利用相似理论的基本原理,导出了此问题的全部准则,并分析了它的流体动力相似问题。本文首次提出了采场实用的复合欧拉准则(Eu'),并再次论证了湍... 本文针对几何边界复杂、流态分布复杂和重力作用与机械压力p相当的复杂采场流场,利用相似理论的基本原理,导出了此问题的全部准则,并分析了它的流体动力相似问题。本文首次提出了采场实用的复合欧拉准则(Eu'),并再次论证了湍流度非独立性的特点。 展开更多
关键词 采场 流场相似 湍流度 流场 流体动力
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Flow equation and similarity criterion during centrifugal casting in micro-channel 被引量:2
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作者 任明星 王国田 +2 位作者 李邦盛 王振龙 傅恒志 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2014年第5期1506-1511,共6页
Liquid metal filling flow process in the microscale during the centrifugal casting process was studied by means of similar physical simulation. The research was focused on derived similarity criterion. Based on the tr... Liquid metal filling flow process in the microscale during the centrifugal casting process was studied by means of similar physical simulation. The research was focused on derived similarity criterion. Based on the traditional flow equations, the flow equation and the Bernoulli's equation for liquid metal flows in micro-scale space were derived, which provides a mathematical model for numerical simulation of micro-scale flow. In the meanwhile, according to the micro-flow equation and the similarity theory, the similarity criterion for the physical simulation of the mold filling behaviors was presented under centrifugal force field, so as to achieve the visual observation and quantitative analysis of micro-flow process. 展开更多
关键词 MICRO-CHANNEL MICRO-FLOW centrifugal force field similarity criterion
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一种水下航行器燃气涡轮机性能模拟试验方法
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作者 陈刚 师海潮 +1 位作者 伊进宝 赵海涛 《鱼雷技术》 2011年第1期77-80,共4页
针对以往水下航行器动力系统设计试验中的不足,通过分析水下航行器涡轮机的基本原理,利用空气动力学和流场相似理论,对涡轮机性能模拟试验原理和方法进行了探讨,提出了一种通过燃气涡轮机低工况性能模拟试验来验证设计工况的试验方法,... 针对以往水下航行器动力系统设计试验中的不足,通过分析水下航行器涡轮机的基本原理,利用空气动力学和流场相似理论,对涡轮机性能模拟试验原理和方法进行了探讨,提出了一种通过燃气涡轮机低工况性能模拟试验来验证设计工况的试验方法,旨在为涡轮机的性能试验验证提供理论基础,同时为涡轮机的试验条件建设提供参考。 展开更多
关键词 水下航行器 燃气涡轮机 空气动力学 流场相似理论 试验方法
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Experimental Study on Jet Blast at Laboratory Scale
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作者 Masato Taguchi Naoki Semba +2 位作者 Koichi Mori Yoshiaki Nakamura Keiichi Ishiko 《Journal of Energy and Power Engineering》 2014年第8期1386-1392,共7页
The flow field of 3D (three-dimensional) wall-jet is investigated. Jet-blast from airplane is simulated by wall-jet setup using a sonic nozzle at a laboratory scale. Farfield velocity and fluctuation distributions a... The flow field of 3D (three-dimensional) wall-jet is investigated. Jet-blast from airplane is simulated by wall-jet setup using a sonic nozzle at a laboratory scale. Farfield velocity and fluctuation distributions are measured by using X-type hot wire anemometer at four measurement planes. As a result, the flow properties of streamwise component are consistent with data which are obtained in previous researches. The secondary flow is also measured on each measurement plane. Reynolds stresses, v'v' and w' w', are analyzed from the fluctuation of the secondary flow. The law of similarity is observed in the dimensionless distributions of mean velocity and fluctuation. However, the distributions in nearer field (i.e., in the measurement plane at X/D = 100) tend to disobey the similarity law, especially in the cases of fluctuation. It seems that jet-blast is not fully developed by reaching X/D = 100. The experimental results are compared with computational results which are obtained by CFD (computational fluid dynamics) with SST (shear-stress transport) turbulence model. And it is shown that the results by the simulation with SST turbulence model do not follow the similarity law. The present database of the Reynolds stresses is critically important for development of a new turbulence model of RANS (reynolds-averaged navier-atokes) simulations on wall-jet. 展开更多
关键词 Experimental fluid dynamics CFD 3D wall jet Reynolds stress secondary flow
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