Volume 32 Issue 8
Aug.  2020
Turn off MathJax
Article Contents
Chen Yong, Lu Daju, Xie Weiming, et al. Unsteady characteristics of aerodynamic loads on a turret[J]. High Power Laser and Particle Beams, 2020, 32: 081001. doi: 10.11884/HPLPB202032.200113
Citation: Chen Yong, Lu Daju, Xie Weiming, et al. Unsteady characteristics of aerodynamic loads on a turret[J]. High Power Laser and Particle Beams, 2020, 32: 081001. doi: 10.11884/HPLPB202032.200113

Unsteady characteristics of aerodynamic loads on a turret

doi: 10.11884/HPLPB202032.200113
  • Received Date: 2020-05-08
  • Rev Recd Date: 2020-08-05
  • Publish Date: 2020-08-13
  • IDDES coupled with J-B model and dual time step LU-SGS method has been adopted to carry out numerical simulation research on unsteady aerodynamic loads on a turret. Flow around the turret will separate, and the separation angle at the zenith is greater than 90°. When the flow bypasses the turret, unsteady flow field structures such as horseshoe vortex and shedding vortex street will form, resulting in unsteady aerodynamic loads. Power spectral density of pulsating static pressure at the zenith lies in the inertial sub-region of isotropic and uniform turbulence at 1.6-40.0 kHz, which basically satisfies Kolmogrov’s −5/3 law. Aerodynamic force is mainly drag force, fluctuation amplitude of transverse force is large, while aerodynamic moment is mainly pitching moment, fluctuation amplitude of rolling moment is also large, but yaw moment can be ignored. The power spectra of aerodynamic force and moment are mainly concentrated below 1 kHz, there are obvious peak frequencies, and the dominant frequency is about 230 Hz (Strouhal number is 0.15). At the beginning of the design of the acquisition tracking pointing (ATP) system, unsteady characteristics of aerodynamic loads on the turret should be considered, and resonant failure problem caused by peak frequencies, especially the dominant frequency, should be avoided.
  • loading
  • [1]
    关奇, 杜太焦, 陈志华, 等. 亚声速球/柱尾流对激光传输影响的数值模拟[J]. 红外与激光工程, 2017, 46:0906005. (Guan Qi, Du Taijiao, Chen Zhihua, et al. Numerical simulation of laser propagation effects through subsonic hemispherical/cylindrical wake[J]. Infrared and Laser Engineering, 2017, 46: 0906005 doi: 10.3788/IRLA201746.0906005
    [2]
    董航, 徐明. 转塔气动光学效应时空特性[J]. 光学学报, 2018, 38:1001002. (Dong Hang, Xu Ming. Space-time characteristics of the aero-optical effect around a turret[J]. Acta Optica Sinica, 2018, 38: 1001002 doi: 10.3788/AOS201838.1001002
    [3]
    Gordeyev S, Jumper E. Fluid dynamics and aero-optics of turrets[J]. Progress in Aerospace Sciences, 2010, 46: 388-400. doi: 10.1016/j.paerosci.2010.06.001
    [4]
    Mathews E, Wang K, Wang M, et al. LES analysis of hemisphere-on-cylinder turret aero-optics[C]//52nd Aerospace Sciences Meeting. 2014.
    [5]
    Arad E, Weidenfeld M. Aero-optic calculations of a spherical turret at transonic flow[C]//55th AIAA Aerospace Sciences Meeting. 2017.
    [6]
    Reynolds T, Saunders D, Presdorf T, et al. Effect of geometric modifications on the flow field of a turret[C]//50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2012.
    [7]
    Morgan P E, Visbal M R. Numerical simulations investigating control of flow over a turret[C]//47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2009.
    [8]
    Mathews E, Wang K, Wang M, et al. Numerical investigation of aero-optical distortions over a hemisphere-on-cylinder turret with gaps[C]//46th AIAA Plasmadynamics and Lasers Conference. 2015.
    [9]
    张露, 李杰. 基于RANS/LES方法的超声速底部流场数值模拟[J]. 航空学报, 2017, 38:120102. (Zang Lu, Li Jie. Numerical simulations of supersonic base flow field based on RANS/LES approaches[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38: 120102
    [10]
    Hu J, Xuan H B, Kwok K C S, et al. Study of wind flow over a 6 m cube using improved delayed detached eddy simulation[J]. Journal of Wind Engineering & Industrial Aerodynamics, 2018, 179: 463-474.
    [11]
    Spalart P R, Jou W H, Strelets M, et al. Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach[J]. Advances in DNS/LES, 1997: 137-148.
    [12]
    Spalart P R, Deck S, Shur M L, et al. A new version of detached-eddy simulation, resistant to ambiguous grid densities[J]. Theoretical and Computational Fluid Dynamics, 2006, 20: 181-195. doi: 10.1007/s00162-006-0015-0
    [13]
    Shur M L, Spalart P R, Strelets M K, et al. A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities[J]. International Journal of Heat and Fluid Flow, 2008, 29: 1638-1649. doi: 10.1016/j.ijheatfluidflow.2008.07.001
    [14]
    Jin G, Braza M. Two-equation turbulence model for unsteady separated flows around airfoils[J]. Journal of American Institute of Aeronautics and Astronautics, 1994, 32(11): 2316-2320. doi: 10.2514/3.12292
    [15]
    Menter F R, Sunnyvale E I. Zonal two equation k-ω turbulence models for aerodynamic flows[C]//24th Fluid Dynamics Conference. 1993.
    [16]
    Jameson A, Yoonf S. Lower-upper implicit schemes with multiple grids for the Euler equations[J]. Journal of American Institute of Aeronautics and Astronautics, 1987, 25(7): 929-935. doi: 10.2514/3.9724
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(6)

    Article views (1077) PDF downloads(46) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return