Computation and measurement of the flow in axial flow fans with skewed blades

被引:81
作者
Beiler, MG [1 ]
Carolus, TH [1 ]
机构
[1] Univ Siegen, Siegen, Germany
来源
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1999年 / 121卷 / 01期
关键词
D O I
10.1115/1.2841234
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A numerical analysis of the flow in axial flow fans with skewed blades has been conducted to study the three-dimensional flow phenomena pertaining to this type of blade shape. The particular fans have a low pressure rise and are designed without stator. Initial studies focused on blades skewed in the circumferential direction, followed by investigations of blades swept ill the direction of the blade chord. A Navier-Stokes code was used to investigate the flow. The simulation results of several fans were validated experimentally. The three-dimensional velocity field was measured in the fixed frame of reference with a triple sensor hot-film probe. Total pressure distribution measurements were performed with a fast response total pressure probe. The results were analyzed, lending to a design method for fans with swept blades. Forward swept fans designed accordingly exhibited good aerodynamic performance. The sound power level, measured on an acoustic fan test facility, improved.
引用
收藏
页码:59 / 66
页数:8
相关论文
共 21 条
[11]  
Dixon SL., 1978, Fluid mechanics, thermodynamics of turbomachinery, V3rd
[12]  
Eck B., 1972, Ventilatoren
[13]  
GODWIN WR, 1957, 4062 NACA TN
[14]  
HORLOCK J, 1958, AXIAL FLOW COMPRESSO
[15]  
KUCHEMANN D, 1952, 2935 AER RES COUNC
[17]  
MOHAMMAD KP, 1977, 77FE1 ASME
[18]   UNDUCTED FAN AERODYNAMIC DESIGN [J].
SMITH, LH .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1987, 109 (03) :313-324
[19]  
SMITH LH, 1963, J BASIC ENG, V9, P401
[20]  
Thwaites B., 1960, INCOMPRESSIBLE AEROD