Experimental verification and numerical simulation of a vortex flowmeter at low Reynolds numbers

被引:6
|
作者
Koncar, B. [1 ,2 ]
Sotosek, J. [1 ,2 ]
Bajsic, I. [3 ]
机构
[1] Jozef Stefan Inst, Ljubljana, Slovenia
[2] Univ Ljubljana, Fac Math & Phys, Ljubljana, Slovenia
[3] Univ Ljubljana, Fac Mech Engn, Ljubljana, Slovenia
关键词
Vortex flowmeter; Shedding frequency; Experimental verification; Numerical simulation; Low Reynolds number; FLOW-RATE; INFLUENCE QUANTITIES; PRESSURE; IDENTIFICATION; SENSOR; BODY;
D O I
10.1016/j.flowmeasinst.2022.102278
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This study presents experimental verification and numerical simulations of a vortex flow meter in the Reynolds number range between 8300 and 50,000. A custom-designed bluff body with a wedge back shape was used in the flowmeter. A shedding frequency of the flowmeter was measured in an air duct using a hot-film probe. To evaluate the accuracy of the flowmeter, a measurement uncertainty analysis was performed. Numerical simu-lations of the vortex flowmeter were performed with the open source code OpenFOAM. Transient simulations of periodic vortex shedding behind the bluff body were performed using different simulation methods depending on the pipe Reynolds number, such as Direct Numerical Simulation (DNS), Large Eddy Simulation (LES) and Un-steady Reynolds Averaged Navier Stokes (URANS) method. The simulated vortex shedding frequencies matched the experimental data very well. Experiments and simulations demonstrated a clear linear dependence of the shedding frequency on the volumetric flow rate over the entire range of Reynolds numbers. In addition, nu-merical simulations were used to study the main mechanisms of vortex formation and shedding behind the considered bluff body.
引用
收藏
页数:10
相关论文
共 50 条
  • [1] Direct numerical simulation and experimental verification for low Reynolds number circular free jet
    Nakashima, K
    Yuu, S
    KAGAKU KOGAKU RONBUNSHU, 1997, 23 (06) : 870 - 877
  • [2] Numerical simulation of two dimensional vortex-induced vibrations of an elliptic cylinder at low Reynolds numbers
    Hasheminejad, Seyyed M.
    Jarrahi, Miad
    COMPUTERS & FLUIDS, 2015, 107 : 25 - 42
  • [3] Experimental Investigation of Transverse and Vortex Gust Encounters at Low Reynolds Numbers
    Biler, Hulya
    Sedky, Girguis
    Jones, Anya R.
    Saritas, Murat
    Cetiner, Oksan
    AIAA JOURNAL, 2021, 59 (03) : 786 - 799
  • [4] Numerical modeling and experimental verification of a low fluid flow inductive flowmeter
    Drexler, P.
    Fiala, P.
    Kadlec, R.
    Londak, P.
    Madrova, T.
    Klima, M.
    Zukal, J.
    FLOW MEASUREMENT AND INSTRUMENTATION, 2021, 78
  • [5] NUMERICAL SIMULATION OF STEADY FLOW OF VORTEX FLOWMETER
    Zhao, Yan-Juan
    Zhang, Yu-Liang
    Zhang, Chen-Liang
    FRONTIERS IN HEAT AND MASS TRANSFER, 2021, 17
  • [6] Numerical prediction of the response of a vortex-excited cylinder at low Reynolds numbers
    Meling, TS
    Dalheim, J
    PROCEEDINGS OF THE SEVENTH (1997) INTERNATIONAL OFFSHORE AND POLAR ENGINEERING CONFERENCE, VOL III, 1997, 1997, : 702 - 709
  • [7] Vortex Shedding of an Airfoil at Low Reynolds Numbers
    Yarusevych, Serhiy
    Boutilier, Michael S. H.
    AIAA JOURNAL, 2011, 49 (10) : 2221 - 2227
  • [8] Direct numerical simulation of deformable rising bubbles at low Reynolds numbers
    Zhang, Lingxin
    Peng, Kai
    Shao, Xueming
    Deng, Jian
    PHYSICS OF FLUIDS, 2021, 33 (11)
  • [9] Experimental and numerical determination of micropropulsion device efficiencies at low Reynolds numbers
    Ketsdever, AD
    Clabough, MT
    Gimelshein, SF
    Alexeenko, A
    AIAA JOURNAL, 2005, 43 (03) : 633 - 641
  • [10] Experimental and numerical determination of micropropulsion device efficiencies at low reynolds numbers
    Ketsdever, Andrew D.
    Clabough, Michael T.
    Gimelshein, Sergey F.
    Alexeenko, Alina
    AIAA Journal, 2005, 43 (03): : 633 - 641