Experimental Investigation of the Aerodynamic Interaction Between Ducts and Actuator Discs

被引:0
|
作者
Tang, J. [1 ]
van Bussel, G. J. W. [1 ]
机构
[1] Delft Univ Technol, Wind Energy Res Grp, Kluyverweg 1, NL-2629 HS Delft, Netherlands
来源
WIND ENERGY EXPLOITATION IN URBAN ENVIRONMENT (TURBWIND 2018) | 2019年 / 8卷
关键词
Ducted wind turbine (DWT); Thrust; Axial momentum theory; Duct; Screen; Wind tunnel experiment; WIND;
D O I
10.1007/978-3-030-13531-7_14
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
The present study aims at providing experimental performance analysis of ducted wind turbines (DWTs) through momentum theory. To simplify the DWT model, a screen emulating the rotor is adopted by applying the actuator disc theory. Two duct models and five different screens are employed for different configurations to investigate the aerodynamic performance of the DWT in this experimental study. Duct 1 (C-T,C-duct = 0.91) is characterized by an aerofoil-shaped cross-section and duct 2 (C-T,C-duct = 1.17) has a cambered shape. Specifically, the five screens vary in porosity from low (C-T,C-screen = 0.46) to high thrust coefficient (C-T,C-screen = 1.12). Results show that the total thrust coefficient (CT, DWT) varies with screen thrusts and ducts geometry. The aerofoil-shaped duct 1, caused by the non-linear behaviour of the aerodynamic force on an aerofoil-shaped body at increasing angle of attack, is more sensitive to the screen loading compared to duct 2. Thrust on duct 1 is highly dependent on screen thrusts owning to the existence of inward oriented lift, while thrust on cambered plate duct 2 stays constant. The high thrust and solid blockage this duct creates, accelerates the flow through the lesser loaded centre where the screen is located. The data also show that the growth of duct thrust has a positive effect on the overall performance of DWT. Both high screen loading and inappropriate aerofoil shape duct may lead to flow separation which causes the momentum loss for DWT. Moreover, the optimal value of C-T,C-screen = 0.89 for a bare wind turbine doesn't seem apply to the tested DWTs. The optimal value of CT, DWT depends both on duct geometry and the screen loading. The velocity measurements further indicate that flow separation occurs at the duct 1 external (pressure) surface, and shows the presence of stalled flow around centre line inside the duct. Finally, a comparison of the pressure distribution of duct with different screen loadings reveals that adding a screen inside duct 1 leads to loss in lift and hence to mass reduction.
引用
收藏
页码:229 / 244
页数:16
相关论文
共 21 条
  • [1] Experimental Investigation on Relations between Flutter Derivatives and Aerodynamic Admittances
    Zhang, Zhitian
    Zhang, Weifeng
    JOURNAL OF BRIDGE ENGINEERING, 2017, 22 (10)
  • [2] Experimental investigation on aerodynamic characteristics of a paraglider wing
    Mashud, Mohammad
    Umemura, Akira
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2006, 49 (163) : 9 - 17
  • [3] Experimental Investigation of the Aerodynamic Roughness Length for Flexible Plants
    Kang, Liqiang
    Zhang, Junjie
    Zou, Xueyong
    Cheng, Hong
    Zhang, Chunlai
    Yang, Zhicheng
    BOUNDARY-LAYER METEOROLOGY, 2019, 172 (03) : 397 - 416
  • [4] Experimental Investigation of the Aerodynamic Roughness Length for Flexible Plants
    Liqiang Kang
    Junjie Zhang
    Xueyong Zou
    Hong Cheng
    Chunlai Zhang
    Zhicheng Yang
    Boundary-Layer Meteorology, 2019, 172 : 397 - 416
  • [5] Experimental investigation of the aerodynamic performance of Flettner rotors for marine applications
    Chen, Wenlong
    Wang, Hanfeng
    Liu, Xiyang
    OCEAN ENGINEERING, 2023, 281
  • [6] Wind Tunnel Experimental Investigation on the Aerodynamic Characteristics of the Multifin Rockets and Missiles
    郝璐
    吴甲生
    Journal of Beijing Institute of Technology, 2005, (03) : 293 - 296
  • [7] Experimental investigation on aerodynamic performance of a flapping wing vehicle in forward flight
    Mazaheri, K.
    Ebrahimi, A.
    JOURNAL OF FLUIDS AND STRUCTURES, 2011, 27 (04) : 586 - 595
  • [8] Extensive design and aerodynamic performance investigation of diffuser augmented wind turbine (DAWT) guided by generalized actuator disc theory
    Dogru, Safak
    Yilmaz, Oktay
    RENEWABLE & SUSTAINABLE ENERGY REVIEWS, 2024, 192
  • [9] Experimental investigation of aerodynamic energy harvester with different interference cylinder cross-sections
    Zhang, L. B.
    Dai, H. L.
    Abdelkefi, A.
    Wang, L.
    ENERGY, 2019, 167 : 970 - 981
  • [10] Aerodynamic experimental investigation and analysis of the flow and thrust generation of the flexible flat flapping wing robot
    Tangudomkit, Kamonrat
    Smithmaitrie, Pruittikom
    2021 SECOND INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION, CONTROL, ARTIFICIAL INTELLIGENCE, AND ROBOTICS (ICA-SYMP), 2021, : 102 - 107