Numerical Studies of Aerodynamic Performance of Gapped Flat Plates at High Angle of Attack

被引:0
|
作者
Tian, De [1 ]
He, Wei [1 ]
Wang, Weilong [1 ]
机构
[1] North China Elect Power Univ, State Key Lab Alternate Elect Power Syst Renewabl, Beijing 102206, Peoples R China
关键词
gapped flat plate; aerodynamic performance; pressure coefficient; numerical simulation; SEPARATED FLOW;
D O I
10.4028/www.scientific.net/AMM.268-270.1172
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In order to study the influence of gap to wind loads on the solar panel, aerodynamic performance of normal flat plate was simulated by various turbulence models with high Reynolds numbers. Time averaged mean drag coefficients and Strouhal numbers were analyzed and compared with other researchers' simulated and experimental results. The flow characteristics of 2D gapped flat plates with different gap sizes at high angle of attack were simulated based on Reynolds stress equation model. Time averaged mean pressure coefficients and Strouhal numbers of gapped flat plates with different gap sizes were compared. The corresponding influences of gap sizes to the pressure coefficients of gapped flat plates were obtained. The simulated results provide theoretical support for the engineering design of the solar panels.
引用
收藏
页码:1172 / 1176
页数:5
相关论文
共 50 条
  • [1] Numerical analysis of windmill blade aerodynamic performance at large attack angle
    Li, Yankai
    Fan, Qinyin
    Dong, Fei
    Guo, Chenhai
    Jiang, Shuli
    Taiyangneng Xuebao/Acta Energiae Solaris Sinica, 2010, 31 (12): : 1639 - 1643
  • [2] Aerodynamic characteristics of flat plates with various angles of attack in oscillatory flow
    Grad. Sch. of Nat. Sci. and Eng., Kanazawa University, 2-40-20 Kodatsuno, Kanazawa, Ishikawa 920, Japan
    不详
    不详
    JSME Int J Ser B, 1 (214-220):
  • [3] Aerodynamic modeling of spatial maneuvering aircraft at high angle of attack
    Wang, Qing
    He, Kai-Feng
    Qian, Wei-Qi
    Mao, Zhong-Jun
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2004, 25 (05): : 447 - 450
  • [4] Effects of average attack angle and amplitude on aerodynamic performance of an oscillating airfoil
    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing
    100191, China
    Tuijin Jishu, 9 (1288-1294):
  • [5] Effect of disk angle-of-attack on aerodynamic performance of small propellers
    Serrano, David
    Ren, Max
    Qureshi, Ahmed Jawad
    Ghaemi, Sina
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 : 901 - 914
  • [6] A vortex force study for a flat plate at high angle of attack
    Li, Juan
    Wu, Zi-Niu
    JOURNAL OF FLUID MECHANICS, 2016, 801 : 222 - 249
  • [7] Numerical simulation of effect of attack angle on performance of SFRJ
    Xie, A.-Y. (xieaiyuan_njust@163.com), 1600, Journal of Solid Rocket Technology, P.O. Box 120, Xi'an, 710025, China (36):
  • [8] Engine thrust effects on rocket aerodynamic characteristics at high angle of attack
    Logan, William V.
    Davis, Roger L.
    Sarigul-Klijn, Nesrin
    Sarigul-Klijn, Marti
    JOURNAL OF SPACECRAFT AND ROCKETS, 2007, 44 (02) : 338 - 346
  • [9] Subsonic steady, unsteady aerodynamic calculation for wings at high angle of attack
    Yang, Y.
    Ye, Z.
    Zhao, L.
    Congress of the International Council of the Aeronautical Sciences - ICAS Proceedings, 1990,
  • [10] Purely aerodynamic pitch control for high-angle-of-attack missiles
    Kim, Yoonsoo
    Kim, Byoung Soo
    38TH ANNUAL CONFERENCE ON IEEE INDUSTRIAL ELECTRONICS SOCIETY (IECON 2012), 2012, : 5584 - 5588