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复杂物理域流场数值模拟软件—CASFLOW的开发 被引量:3
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作者 季路成 钟文涛 徐建中 《工程热物理学报》 EI CAS CSCD 北大核心 2000年第6期700-702,共3页
本文开发了CFD软件—CASFLOW,其目标是为燃气轮机气动仿真系统提供一个CFD软件平台。本工作是阶段性的,为使CASFLOW软件最终成为功能强大、通用性强的研究工具,还有大量的工作需要继续,尤其是校验和标定。初步... 本文开发了CFD软件—CASFLOW,其目标是为燃气轮机气动仿真系统提供一个CFD软件平台。本工作是阶段性的,为使CASFLOW软件最终成为功能强大、通用性强的研究工具,还有大量的工作需要继续,尤其是校验和标定。初步工作已经显示出CASFLOW处理复杂物理域内复杂流动的能力。 展开更多
关键词 流体动力学 物理域 流场数值模拟软件 软件开发
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Numerical simulation of flow field of single-hole oxygen lance jet
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作者 LIU Kun HAN Ren-zhi BAO Li-ming 《Journal of Energy and Power Engineering》 2007年第1期22-28,共7页
The numerical simulation of jet flow field in Laval tube was carried out first by commercial software CFX4.4, and it is used to determine inlet pressure condition out of nozzle in order to its numerical simulation. Th... The numerical simulation of jet flow field in Laval tube was carried out first by commercial software CFX4.4, and it is used to determine inlet pressure condition out of nozzle in order to its numerical simulation. The decay rule of jet middle line velocity of axial symmetry turbulence jet and cross section's expand situation out of the tube in different stagnation pressure and surrounding temperature were analyzed systematically. The result showed that K-e model is suitable for numerical simulation. The conclusion will have important guide and referent function to research of two important craft parameters, impact depth and the impact area which are related to steel-making production practice. 展开更多
关键词 Laval tube axis symmetry turbulence jet simulation
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Effects of Measuring Positions on the Measured Aerodynamic Performance of a Centrifugal Compressor 被引量:1
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作者 Hongwei MA Jun ZHANG 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第2期110-114,共5页
This paper performs a numerical simulation of three-dimensional flow field in a centrifugal compressor with long inlet and outlet pipes using CFX software.By arranging virtual probes at different positions in both inl... This paper performs a numerical simulation of three-dimensional flow field in a centrifugal compressor with long inlet and outlet pipes using CFX software.By arranging virtual probes at different positions in both inlet and outlet planes,the aerodynamic performance of the centrifugal compressor is measured and compared with each other.Then effects of measuring positions on measurement results are discussed.The results show that it will generate notable measuring errors of the pressure ratio and efficiency if the inlet total pressure is measured using a single-point probe.The inlet total pressure data can be accurate when they are measured using a 3-point rake.The outlet total pressure and total temperature data can not be accurate if they are respectively measured at one circumferential position even using a multi-point rake.Increasing tangential measuring positions at the outlet is effective to improve the test accuracy.When the outlet total pressure and total temperature are respectively measured at 3 tangential positions,the data can be almost accurate. 展开更多
关键词 centrifugal compressor aerodynamics performance measuring error measurement position probe.
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