Measurements of fluctuating lift forces on rectangular cylinders in turbulent flow

被引:15
作者
Yang, Yang [1 ,2 ]
Li, Mingshui [2 ]
Kim, Ho-Kyung [3 ]
Li, Ming [2 ]
机构
[1] Seoul Natl Univ, Korea Bridge Design & Engn Res Ctr, Seoul 08826, South Korea
[2] Southwest Jiaotong Univ, Res Ctr Wind Engn, Chengdu 610031, Peoples R China
[3] Seoul Natl Univ, Dept Civil & Environm Engn, Seoul 08826, South Korea
基金
中国国家自然科学基金; 新加坡国家研究基金会;
关键词
AERODYNAMIC ADMITTANCE; SURFACE THEORY; SPECTRA;
D O I
10.1063/1.5125657
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The fluctuating lift on a rectangular cylinder induced by turbulent flow is investigated by force measurement experiments. A square uniform grid is installed downstream of the entrance of the working section of the wind tunnel to generate approximately homogeneous and isotropic turbulence. The rectangular cylinder models of two different cross sections (width to depth ratio BID = 5, 10) are tested in the experiments. Each rectangular cross section has two aspect ratios (length to width ratio theta = 1, 7) and a fixed width (B = 0.15 m). The measurements include the spectra of fluctuating lift force and vertical turbulent velocity component. From these measurements, the experimental values of generalized transfer functions of these rectangular cylinder models are obtained, which are compared with the calculated values based on three aerodynamic force theories. The one-wavenumber transfer functions and the spanwise influence terms of these rectangular cylinders are used in the calculations, which were determined by the pressure measurement experiments in the previous work. Comparisons of the measured and calculated values of generalized transfer functions demonstrate that the three-dimensional theory is satisfactory and confirm that the one-wavenumber transfer functions and spanwise influence terms determined by the pressure measurements are valid. The results also show that both the two-dimensional theory and the strip theory would overestimate the generalized transfer function, but for the rectangular cylinder with the larger aspect ratio, the strip theory is very close to the three-dimensional theory. The one-wavenumber transfer functions of these rectangular cylinders are therefore determined based on the strip theory. This indicates that the approximate approach to determination of the one-wavenumber transfer function, which was proposed for an airfoil in the previous work, could also be applicable to bluff bodies. Published under license by AIP Publishing.
引用
收藏
页数:13
相关论文
共 36 条
[1]   Effect of turbulence on the drag and lift of a particle [J].
Bagchi, P ;
Balachandar, S .
PHYSICS OF FLUIDS, 2003, 15 (11) :3496-3513
[2]   Wind tunnel study of the wind turbine interaction with a boundary-layer flow: Upwind region, turbine performance, and wake region [J].
Bastankhah, M. ;
Porte-Agel, F. .
PHYSICS OF FLUIDS, 2017, 29 (06)
[3]  
Blake W.K., 1986, MECH FLOW INDUCED SO
[4]  
Clementson G., 1950, THESIS
[5]  
Davenport A.G., 1962, J STRUCT ENG, V88, P233, DOI [10.1061/JSDEAG.0000773, DOI 10.1061/JSDEAG.0000773]
[6]   THE DYNAMIC RESPONSE OF A LARGE AIRPLANE TO CONTINUOUS RANDOM ATMOSPHERIC DISTURBANCES [J].
DIEDERICH, FW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (10) :917-930
[7]   A THEORY OF THE RESPONSE OF AIRPLANES TO RANDOM ATMOSPHERIC TURBULENCE [J].
ETKIN, B .
JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (07) :409-420
[8]  
Filotas L.T., 1969, 139 UTIAS
[9]   LIFTING SURFACE THEORY FOR PROBLEM OF AN ARBITRARILY YAWED SINUSOIDAL GUST INCIDENT ON A THIN AEROFOIL IN INCOMPRESSIBLE FLOW [J].
GRAHAM, JMR .
AERONAUTICAL QUARTERLY, 1970, 21 :182-&
[10]   LIFTING-SURFACE THEORY FOR RECTANGULAR WING IN NON-STATIONARY FLOW [J].
GRAHAM, JMR .
AERONAUTICAL QUARTERLY, 1971, 22 (FEB) :83-&