Experimental and numerical study of transient flow in a centrifugal pump during startup

被引:54
作者
Li, Zhifeng [1 ,2 ]
Wu, Peng [1 ,2 ]
Wu, Dazhuan [1 ,2 ]
Wang, Leqin [1 ,2 ]
机构
[1] Zhejiang Univ, Dept Chem & Biol Engn, Inst Proc Equipment, Hangzhou 310027, Peoples R China
[2] Minist Educ, Engn Res Ctr High Pressure Proc Equipment & Safet, Hangzhou 310027, Peoples R China
基金
中国博士后科学基金; 中国国家自然科学基金;
关键词
Numerical simulation; Experimental test; Transient flow; Centrifugal pump; Starting period; OPERATING-CONDITIONS; RAPID CHANGE; CIRCULAR-CYLINDER; DYNAMIC MESH; BEHAVIOR;
D O I
10.1007/s12206-011-0107-7
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Transient characteristics and flows in a centrifugal pump during its starting period were experimentally and numerically investigated. The two-dimensional particle image velocimetry technique was used to capture transient flow evolutions in the pump's diffuser. A new dynamic slip region mAhod that combines the dynamic mesh method with the non-conformal grid boundaries is proposed to resolve the transient flows caused by the started impeller. Numerical self-coupling was realized by establishing a circulation pipe system along with the pump model equivalent to the experimental pump system. Numerical and experimental results agree well in both explicit characteristics and internal transient flow structures, confirming the validity of the proposed method. Analysis of the instantaneous flow in the impellers indicates that for the early stage of the startup, the transient vortex evolution between blades is the main reason for the transient head coefficient being lower than the steady state value. The reversed flow at the blade inlet is a less important reason for this effect. In later stages, the weakening of the intensity of the spatial vortex visible on S2, and the main flow stream are the main reasons for the explicit performance slowly rebounding to the steady value.
引用
收藏
页码:749 / 757
页数:9
相关论文
共 29 条
[1]   UNSTEADY EULER ALGORITHM WITH UNSTRUCTURED DYNAMIC MESH FOR COMPLEX-AIRCRAFT AERODYNAMIC ANALYSIS [J].
BATINA, JT .
AIAA JOURNAL, 1991, 29 (03) :327-333
[2]   Modelling turbulent flow past a circular cylinder by RANS, URANS, LES and DES [J].
Benim, A. C. ;
Pasqualotto, E. ;
Suh, S. H. .
PROGRESS IN COMPUTATIONAL FLUID DYNAMICS, 2008, 8 (05) :299-307
[3]  
Bolpaire S., 2000, THESIS ECOLE NATL SU
[4]   Transient behavior of turbomachineries: Applications to radial flow pump startups [J].
Dazin, Antoine ;
Caignaert, Guy ;
Bois, Gerard .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2007, 129 (11) :1436-1444
[5]   FINITE VOLUME METHOD FOR PREDICTION OF FLUID-FLOW IN ARBITRARILY SHAPED DOMAINS WITH MOVING BOUNDARIES [J].
DEMIRDZIC, I ;
PERIC, M .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 1990, 10 (07) :771-790
[6]  
Ghelici N., 1993, THESIS ECOLE NATL SU
[7]  
GOSWAMI A, 1991, AIAA, V91, P1589
[8]   CENTRIFUGAL PUMP PERFORMANCE DURING TRANSIENT OPERATION [J].
LEFEBVRE, PJ ;
BARKER, WP .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1995, 117 (01) :123-128
[9]  
LI JW, 2008, SHUILI FADIAN XUEBAO, V27, P148
[10]  
LI JW, 2008, SHUILI FADIAN XUEBAO, V27, P147