Turn off MathJax
Article Contents
WANG Y F, QIN Q H, GUAN R Q, et al. Experimental study and statistical analysis of flow field pulsation of spiked cylinder[J]. Journal of Experiments in Fluid Mechanics, doi: 10.11729/syltlx20220078
Citation: WANG Y F, QIN Q H, GUAN R Q, et al. Experimental study and statistical analysis of flow field pulsation of spiked cylinder[J]. Journal of Experiments in Fluid Mechanics, doi: 10.11729/syltlx20220078

Experimental study and statistical analysis of flow field pulsation of spiked cylinder

doi: 10.11729/syltlx20220078
  • Received Date: 2022-08-18
  • Accepted Date: 2022-10-10
  • Rev Recd Date: 2022-09-16
  • Available Online: 2023-03-14
  • The cylinder with a pointed spike and the spiked cylinder with aerodome were investigated under the condition of Ma = 2.2 incoming flow using a direct-connected wind tunnel and a high-speed schlieren system. The experimental results were statistically analyzed to investigate the unsteady flow field pulsation of the spiked cylinder under supersonic incoming flow. Based on the transient data, the typical structure and evolution of the flow field were first interpreted. The convergence of the residuals was then used to assess the dependability of the statistical results. Finally, the pulsation characteristics of the flow field were further analyzed in terms of the time-averaged and pulsating flow fields. The results show that there is unsteady pulsation in the spiked cylinder flow field under the condition of the supersonic incoming flow, which is more intense in the case of the cylinder with a pointed spike and attenuated in the case of the spiked cylinder with aerodome, demonstrating the suppression of unsteady pulsation in the flow field by the aerodome.
  • loading
  • [1]
    STEWARTSON K. On the linearized potential theory of unsteady supersonic motion[J]. The Quarterly Journal of Mechanics and Applied Mathematics, 1950, 3(2): 182–199. doi: 10.1093/qjmam/3.2.182
    [2]
    CLEMENS N T, NARAYANASWAMY V. Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions[J]. Annual Review of Fluid Mechanics, 2014, 46: 469–492. doi: 10.1146/annurev-fluid-010313-141346
    [3]
    SCHUELEIN E. Wave drag reduction approach for blunt bodies at high angles of attack: proof-of-concept experiments[C]//Proc of the 4th Flow Control Conference. 2008. doi: 10.2514/6.2008-4000
    [4]
    GNEMMI P, SRULIJES J, ROUSSEL K, et al. Flowfield around spike-tipped bodies for high attack angles at Mach 4.5[J]. Journal of Spacecraft and Rockets, 2003, 40(5): 622–631. doi: 10.2514/2.6910
    [5]
    ALEXANDER S. Results of tests to determine the effect of a conical windshield on the drag of a bluff body at supersonic speeds[R]. NACA-RM-L6K08a, 1947.
    [6]
    STALDER J R, NIELSEN H V. Heat transfer from a hemisphere-cylinder equipped with flow-separation spikes [R]. NACA-TN-3287, 1954.
    [7]
    CRAWFORD D H. Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8[R]. NASA TN D-118, 1959.
    [8]
    WOOD C J. Hypersonic flow over spiked cones[J]. Journal of Fluid Mechanics, 1962, 12(4): 614–624. doi: 10.1017/s0022112062000427
    [9]
    HOLDEN M S. Experimental studies of separated flows at hypersonic speeds. I - Separated flows over axisymmetric spiked bodies[J]. AIAA Journal, 1966, 4(4): 591–599. doi: 10.2514/3.3494
    [10]
    AHMED M Y M, QIN N. Forebody shock control devices for drag and aero-heating reduction: a comprehensive survey with a practical perspective[J]. Progress in Aerospace Sciences, 2020, 112: 100585. doi: 10.1016/j.paerosci.2019.100585
    [11]
    AHMED M Y M, QIN N. Recent advances in the aerothermodynamics of spiked hypersonic vehicles[J]. Progress in Aerospace Sciences, 2011, 47(6): 425–449. doi: 10.1016/j.paerosci.2011.06.001
    [12]
    HUANG W, CHEN Z, YAN L, et al. Drag and heat flux reduction mechanism induced by the spike and its combinations in supersonic flows: a review[J]. Progress in Aerospace Sciences, 2019, 105: 31–39. doi: 10.1016/j.paerosci.2018.12.001
    [13]
    SUN X W, HUANG W, OU M, et al. A survey on numerical simulations of drag and heat reduction mechanism in supersonic/hypersonic flows[J]. Chinese Journal of Aeronautics, 2019, 32(4): 771–784. doi: 10.1016/j.cja.2018.12.024
    [14]
    WANG Z G, SUN X W, HUANG W, et al. Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: a survey[J]. Acta Astronautica, 2016, 129: 95–110. doi: 10.1016/j.actaastro.2016.09.004
    [15]
    HUANG W. A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations[J]. Journal of Zhejiang University-SCIENCE A, 2015, 16(7): 551–561. doi: 10.1631/jzus.A1500021
    [16]
    OU M, YAN L, HUANG W, et al. Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows[J]. International Journal of Heat and Mass Transfer, 2018, 126: 10–31. doi: 10.1016/j.ijheatmasstransfer.2018.05.013
    [17]
    LI S B, HUANG W, LEI J, et al. Drag and heat reduction mechanism of the porous opposing jet for variable blunt hypersonic vehicles[J]. International Journal of Heat and Mass Transfer, 2018, 126: 1087–1098. doi: 10.1016/j.ijheatmasstransfer.2018.06.054
    [18]
    XUE Y, WANG L, FU S. Detached-eddy simulation of supersonic flow past a spike-tipped blunt nose[J]. Chinese Journal of Aeronautics, 2018, 31(9): 1815–1821. doi: 10.1016/j.cja.2018.06.016
    [19]
    KENWORTHY M A. A study of unstable axisymmetric separation in high speed flows [D]. Blacksburg: Virginia Polytechnic Institute and State University, 1978.
    [20]
    FESZTY D, BADCOCK K J, RICHARDS B E. Driving mechanisms of high-speed unsteady spiked body flows, part I: pulsation mode[J]. AIAA Journal, 2004, 42(1): 95–106. doi: 10.2514/1.9034
    [21]
    FESZTY D, BADCOCK K J, RICHARDS B E. Driving mechanism of high-speed unsteady spiked body flows, part 2: oscillation mode[J]. AIAA Journal, 2004, 42(1): 107–113. doi: 10.2514/1.9035
    [22]
    QIN Q H, GUAN R Q, MA Z, et al. Experimental verification of pulsation suppression over spiked cylinder using standard/double/inverse aerodome[J]. Aerospace Science and Technology, 2021, 116: 106848. doi: 10.1016/j.ast.2021.106848
    [23]
    SAHOO D, DAS S, KUMAR P, et al. Effect of spike on steady and unsteady flow over a blunt body at supersonic speed[J]. Acta Astronautica, 2016, 128: 521–533. doi: 10.1016/j.actaastro.2016.08.005
    [24]
    SAHOO D, KARTHICK S K, DAS S, et al. Shock-related unsteadiness of axisymmetric spiked bodies in supersonic flow[J]. Experiments in Fluids, 2021, 62(4): 89. doi: 10.1007/s00348-020-03130-2
    [25]
    WANG Z A, CHANG J T, WU G W, et al. Experimental investigation of shock train behavior in a supersonic isolator[J]. Physics of Fluids, 2021, 33(4): 046103. doi: 10.1063/5.0047665
    [26]
    COMBS C S, SCHMISSEUR J D, BATHEL B F, et al. Unsteady analysis of shock-wave/boundary-layer interaction experiments at Mach 4.2[J]. AIAA Journal, 2019, 57(11): 4715–4724. doi: 10.2514/1.j058073
    [27]
    SUN Z Z, GAN T, WU Y. Shock-wave/boundary-layer interactions at compression ramps studied by high-speed schlieren[J]. AIAA Journal, 2019, 58(4): 1681–1688. doi: 10.2514/1.J058257
    [28]
    SUN Z Z, MIAO X, JAGADEESH C. Experimental investigation of the transonic shock-wave/boundary-layer interaction over a shock-generation bump[J]. Physics of Fluids, 2020, 32(10): 106102. doi: 10.1063/5.0018763
  • 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(9)  / Tables(2)

    Article Metrics

    Article views (231) PDF downloads(16) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return