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非定常态供应链集成模式——应急物流体分析 被引量:12
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作者 韩景倜 詹亚辉 +1 位作者 徐颖凯 李常富 《空军工程大学学报(自然科学版)》 CSCD 北大核心 2005年第2期92-94,共3页
剖析非定常态下物流供应链及其应急保障物流的结构特征,提出应急物流体的概念和基本模型。应急物流体是构建于国家和企业物流供应链基础上、经集成的特殊物流供应链系统模式。为应急状态下的实时物流供应(RTLS)提供决策支持,为相应研究... 剖析非定常态下物流供应链及其应急保障物流的结构特征,提出应急物流体的概念和基本模型。应急物流体是构建于国家和企业物流供应链基础上、经集成的特殊物流供应链系统模式。为应急状态下的实时物流供应(RTLS)提供决策支持,为相应研究提供新的思路。 展开更多
关键词 非定常态 物流供应 物流体
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Statistical analysis of pressure fluctuations during unsteady flow for low-specific-speed centrifugal pumps 被引量:3
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作者 裴吉 王文杰 袁寿其 《Journal of Central South University》 SCIE EI CAS 2014年第3期1017-1024,共8页
A three-dimensional transient numerical simulation was conducted to study the pressure fluctuations in low-specific-speed centrifugal pumps. The characteristics of the inner flow were investigated using the SST k-ω t... A three-dimensional transient numerical simulation was conducted to study the pressure fluctuations in low-specific-speed centrifugal pumps. The characteristics of the inner flow were investigated using the SST k-ω turbulence model. The distributions of pressure fluctuations in the impeller and the volute were recorded, and the pressure fluctuation intensity was analyzed comprehensively, at the design condition, using statistical methods. The results show that the pressure fluctuation intensity increases along the impeller streamline from the leading edge to the trailing edge. In the impeller passage, the intensity near the shroud is much higher than that near the hub at thc inlet. However, the intensity at the middle passage is almost equal to the intensity at the outlet. The pressure fluctuation intensity is the highest at the trailing edge on the pressure side and near the tongue because of the rotor-stator interaction. The distribution of pressure fluctuation intensity is symmetrical in the axial cross sections of the volute channel. However, this intensity decreases with increasing radial distance. Hence, the pressure fluctuation intensity can be reduced by modifying the geometry of the leading edge in the impeller and the tongue in the volute. 展开更多
关键词 TRANSIENT pressure fluctuation intensity STATISTICS low specific speed centrifugal pump
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Experimental and Numerical Investigation of the Unsteady Tip Leakage Flow in Axial Compressor Cascade 被引量:3
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作者 Chengqing Li Tingfeng Ke +2 位作者 Jingxuan Zhang Hongwu Zhang Weiguang Huang 《Journal of Thermal Science》 SCIE EI CAS CSCD 2013年第2期103-110,共8页
For convenience of both measurement and adjusting the clearance size and incidence, the current research is mainly conducted by experiments on an axial compressor linear cascade. The characteristics and the condition ... For convenience of both measurement and adjusting the clearance size and incidence, the current research is mainly conducted by experiments on an axial compressor linear cascade. The characteristics and the condition under which the unsteadiness of tip leakage flow would occur were investigated by dynamic measuring in different clearances, inlet velocities and incidences. From the experiment it is found that increasing tip clearance size or reducing rotor tip incidence can affect the strength of the tip clearance flow. Then the experimental results also indicate the tip leakage shows instability in certain conditions, and the frequency of unsteadiness is great influenced by inflow angle. The condition of occurrence of tip leakage flow unsteadiness is when the leakage flow is strong enough to reach the pressure side of the adjacent blade. The main cause of tip leakage flow unsteadiness is the tip blade loading. 展开更多
关键词 axial flow compressor linear cascade tip leakage flow UNSTEADY
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Effect of Inlet Guide Vanes on the Performance of Small Axial Flow Fan 被引量:4
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作者 LIU Yang LIN Zhe +3 位作者 LIN Peifeng JIN Yingzi Toshiaki Setoguchi Heuy Dong Kim 《Journal of Thermal Science》 SCIE EI CAS CSCD 2017年第6期504-513,共10页
Effects of the inlet guide vanes on the static characteristics, aerodynamic noise and internal flow characteristics of a small axial flow fan are studied in this work. The inlet guide vanes with different outlet angle... Effects of the inlet guide vanes on the static characteristics, aerodynamic noise and internal flow characteristics of a small axial flow fan are studied in this work. The inlet guide vanes with different outlet angle are designed, which are mounted on the casing and located at the upstream of the impeller of the prototype fan. Both steady and unsteady flow simulations arc performed. The steady flow is simulated by the calculations of Navier-Stokes equa- tions coupled with RNG k-epsilon turbulence model, while the unsteady flow is computed with large eddy simu- lation. According to the theoretical analysis, the inlet guide vanes with outlet angle of 60° are regarded as the op- timal inlet guide vanes. The static characteristic experiment is carried out in a standard test rig and the aerody- namic noise is tested in a semi-anechoic room. Then, performances of the fan with optimal inlet guide vanes are compared with those of the prototype fan. The results show that there is reasonable agreement between the simu- lation results and the experimental data. It is found that the static characteristics of small axial flow fan is im- proved obviously after installing the optimal inlet guide vanes. Meanwhile, the optimal inlet guide vanes have effect on reducing noise at the near field, but have little effect on the noise at the far field. 展开更多
关键词 small axial flow fan inlet guide vanes static characteristics aerodynamic noise internal flow characteristics
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