Wang Xiaopeng, Zhang Chen'an, Zhai Jian, et al. Experimental study on the aero-heating characteristics of waverider in the high enthalpy shock wave tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(4): 52-57. doi: 10.11729/syltlx20190080
Citation: Wang Xiaopeng, Zhang Chen'an, Zhai Jian, et al. Experimental study on the aero-heating characteristics of waverider in the high enthalpy shock wave tunnel[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(4): 52-57. doi: 10.11729/syltlx20190080

Experimental study on the aero-heating characteristics of waverider in the high enthalpy shock wave tunnel

doi: 10.11729/syltlx20190080
  • Received Date: 2019-06-24
  • Rev Recd Date: 2019-07-17
  • Publish Date: 2019-08-25
  • Long-range aerodynamic heating is a key scientific problem. In this paper, the cone-derived waverider is designed firstly and then the characteristics of the heat flux distribution along the leading edge and on the lower surface of the waverider are studied by means of the high enthalpy wind tunnel test and the high temperature chemical non-equilibrium aerodynamic heating numerical calculation. Results show that:The high heat flux mainly concentrates on the small region around the stagnation point and the change of angle of attack (0°~6°) does not have an obvious effect on the high heat flux region at the leading edge, but it induces a significant increase of the heat flux on the lower surface. In addition, the change of the sideslip angle (0°~4°) has a significant effect on the heat flux at the leading edge, so it is not recommended to fly with a large sideslip angle.
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  • [1]
    吕红庆.乘波体结构热响应及防护问题研究[D].哈尔滨: 哈尔滨工程大学, 2010. http://cdmd.cnki.com.cn/article/cdmd-10217-1012266032.htm

    Lyu H Q. Study of thermal response and protection for waverider structure[D]. Harbin: Harbin Engineering Univer-sity, 2010. http://cdmd.cnki.com.cn/article/cdmd-10217-1012266032.htm
    [2]
    周印佳.乘波构型设计及表面热流计算[D].哈尔滨: 哈尔滨工程大学, 2012. http://cdmd.cnki.com.cn/Article/CDMD-10217-1012517871.htm

    Zhou Y J. Design of waverider configuration and calculation of heating rates on the surface[D]. Harbin: Harbin Engineering University, 2012. http://cdmd.cnki.com.cn/Article/CDMD-10217-1012517871.htm
    [3]
    刘建霞, 侯中喜, 陈小庆, 等.高超声速滑翔飞行器气动性能的数值模拟研究[J].国防科技大学学报, 2012, 34(4):22-27. doi: 10.3969/j.issn.1001-2486.2012.04.005

    Liu J X, Hou Z X, Chen X Q, et al. Numerical simulation on the aerodynamic performance of hypersonic glide vehicle[J]. Journal of National University of Defense Technology, 2012, 34(4):22-27. doi: 10.3969/j.issn.1001-2486.2012.04.005
    [4]
    Liu J X, Hou Z X, Chen X Q, et al. Experimental and numerical study on the aero-heating characteristics of blunted waverider[J]. Applied Thermal Engineering, 2013, 51(1-2):301-314. doi: 10.1016/j.applthermaleng.2012.09.026
    [5]
    杨建龙, 刘猛, 阿嵘, 等.高超声速热化学非平衡对气动热环境影响[J].北京航空航天大学学报, 2017, 43(10):2063-2072. http://d.old.wanfangdata.com.cn/Periodical/bjhkhtdxxb201710015

    Yang J L, Liu M, A R. Influence of hypersonic thermo-chemical non-equilibrium on aerodynamic thermal environments[J]. Journal of Beijing University of Aeronautics and Astronau-tics, 2017, 43(10):2063-2072. http://d.old.wanfangdata.com.cn/Periodical/bjhkhtdxxb201710015
    [6]
    董维中, 丁明松, 高铁锁, 等.热化学非平衡模型和表面温度对气动热计算影响分析[J].空气动力学学报, 2013, 31(6):692-698. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201306002

    Dong W Z, Ding M S, Gao T S, et al. The influence of thermo-chemical non-equilibrium model and surface temperature on heat transfer rate[J]. Acta Aerodynamica Sinica, 2013, 31(6):692-698. http://d.old.wanfangdata.com.cn/Periodical/kqdlxxb201306002
    [7]
    Liu Z, Liu J, Ding F, et al. Effect of thermochemical non-equilibrium on the aerodynamics of an osculating-cone wave-rider under different angles of attack[J]. Acta Astronautica, 2017, 139:288-295. doi: 10.1016/j.actaastro.2017.07.013
    [8]
    Liu J, Li K, Liu W Q. High-temperature gas effects on aerodynamic characteristics of waverider[J]. Chinese Journal of Aeronautics, 2015, 28(1):57-65. doi: 10.1016/j.cja.2014.12.004
    [9]
    杨恺, 原志超, 朱强华, 等.高超声速热化学非平衡钝体绕流数值模拟[J].推进技术, 2014, 35(12):1585-1591. http://d.old.wanfangdata.com.cn/Conference/8155863

    Yang K, Yuan Z C, Zhu Q H, el al. Numerical simulation of hypersonic thermochemical nonequilibrium blunt body flows[J]. Journal of Propulsion Technology, 2014, 35(12):1585-1591. http://d.old.wanfangdata.com.cn/Conference/8155863
    [10]
    Pezzella G, Votta R. Finite rate of chemistry effects on the high altitude aerodynamics of an apollo-shaped reentry capsule[R]. AIAA-2009-7306, 2009.
    [11]
    Gao Z X, Jiang C W, Lee C H. Aero-heating study of hypersonic chemical nonequilibrium flows around a reentry blunt body[R]. AIAA-2014-4415, 2014.
    [12]
    Hao J, Wang J Y, Lee C H. Numerical study of hypersonic flows over reentry configurations with different chemical nonequilibrium models[J]. Acta Astronautica, 2016, 126:1-10. doi: 10.1016/j.actaastro.2016.04.014
    [13]
    Suzuki K, Abe T. Thermochemical nonequilibrium viscous shock-layer analysis for a Mars aerocapture vehicle[J]. Journal of Thermophysics and Heat Transfer, 1994, 8(4):773-780. doi: 10.2514/3.611
    [14]
    Inger G R. Nonequilibrium boundary-layer effects on the aerodynamic heating of hypersonic waverider vehicles[J]. Journal of Thermophysics and Heat Transfer, 1995, 9(4):595-604. doi: 10.2514/3.713
    [15]
    Inger G R. Non-equilibrium boundary layer effects on the aerodynamic heating of hypersonic vehicles[J]. Acta Astronau-tica, 1995, 36(4):205-216. doi: 10.1016/0094-5765(95)00101-5
    [16]
    Starkey R P. Design of waverider based re-entry vehicles[R]. AIAA-2005-3390, 2005.
    [17]
    曾卫刚, 李维东, 王发民.平衡气体对乘波体气动力/热特性影响[J].空气动力学学报, 2012, 30(5):566-572, 605. http://www.cqvip.com/QK/95593X/201205/43755638.html

    Zeng W G, Li W D, Wang F M. Equilibrium gas effects on aerodynamic and aerothermal characteristics of waveriders[J]. Acta Aerodynamica Sinica, 2012, 30(5):566-572, 605. http://www.cqvip.com/QK/95593X/201205/43755638.html
    [18]
    耿永兵, 刘宏, 雷麦芳, 等.高升阻比乘波构型优化设计[J].力学学报, 2006, 38(4):540-546. doi: 10.3321/j.issn:0459-1879.2006.04.014

    Geng Y B, Liu H, Lei M F. Optimized design of waverider with high lift over drag ratio[J]. Chinese Journal of Theoretical and Applied Mechanics, 2006, 38(4):540-546. doi: 10.3321/j.issn:0459-1879.2006.04.014
    [19]
    聂春生, 李宇, 黄建栋, 等.高超声速非平衡气动加热试验及数值分析研究[J].中国科学:技术科学, 2018, 48(8):845-852. http://www.cnki.com.cn/Article/CJFDTotal-JEXK201808004.htm

    Nie C S, Li Y, Huang J D, et al. Test of aero-heating in hypersonic non-equilibrium flow and numerical simulation study[J]. Scientia Sinica:Technologica, 2018, 48(8):845-852. http://www.cnki.com.cn/Article/CJFDTotal-JEXK201808004.htm
    [20]
    Gupta R N, Yos J M, Thompson R A, et al. A review of reaction rates and thermodynamic and transport properties for an 11-species air model for chemical and thermal nonequilibrium calculations to 30000K[R]. NASA-TM-101528, 1990.
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