Flow field behavior with Reynolds number variance around a spiked body

被引:4
|
作者
Khurana, Shashank [1 ,4 ]
Suzuki, Kojiro [2 ]
Rathakrishnan, Ethirajan [3 ]
机构
[1] Peking Univ, Coll Engn, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China
[2] Univ Tokyo, Dept Adv Energy, 5-1-5 Kashiwanoha, Kashiwa, Chiba 2778561, Japan
[3] IIT Kanpur, Dept Aerosp Engn, Kanpur 208016, Uttar Pradesh, India
[4] BITS Pilani, Dept Mech Engn, Dubai, U Arab Emirates
来源
MODERN PHYSICS LETTERS B | 2016年 / 30卷 / 30期
关键词
Aerospike; water channel; Reynolds number; flow visualization; vortices;
D O I
10.1142/S0217984916503620
中图分类号
O59 [应用物理学];
学科分类号
摘要
An experimental visualization study was performed to investigate the dependence of the pressure hill height and the influence zone expanse, for flow past a spiked body with different nose configurations, over a Reynolds number range from 2278 to 4405 to establish the vortex shedding process, and applicability in low speed flow regime for effective pressure reduction. It is found that the spike reduces the radius of curvature of the approaching streamline, leading to the deflection of the streamlines towards the shoulder of the basic body, resulting in a narrow zone of the positive pressure hill at the body nose. It is also observed that the pressure hill length and the influence zone expanse decrease with the introduction of spike over the present range of Reynolds numbers. For Reynolds numbers less than 2700, spike with conical nose is found to be more efficient than the spikes with other nose shapes of the present study in reducing the positive pressure at the nose of the blunt body. For higher Reynolds numbers, greater than 2700, the size of the vortex at the junction of the spike and basic body is the largest for the spike with hemispherical nose, and emerges as a potential candidate for application in possible wind-design resistant structures.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] Flow around the revolving propeller blades in low Reynolds number field
    Arai, Nobuyuki
    Yoshida, Hironori
    Hiraoka, Katsumi
    [J]. FEDSM 2007: PROCEEDINGS OF THE 5TH JOINT AMSE/JSME FLUIDS ENGINEERING SUMMER CONFERENCE VOL 1, PTS A AND B, 2007, : 1795 - 1803
  • [2] Comparison of low Reynolds Number k-Ε Models in Predicting Complicated Flow Field Around a Bluff Body
    Yang, Zhigang
    Zhou, Yongxiang
    Zhu, Hui
    Li, Yanlong
    [J]. Tongji Daxue Xuebao/Journal of Tongji University, 2017, 45 (03): : 413 - 419
  • [3] COMPRESSIBLE LOW REYNOLDS NUMBER FLOW AROUND ASPHERE
    KASSOY, DR
    ADAMSON, TC
    MESSITER, AF
    [J]. PHYSICS OF FLUIDS, 1966, 9 (04) : 671 - &
  • [4] A numerical investigation about the effects of Reynolds number on the flow around an appended axisymmetric body of revolution
    Posa, Antonio
    Balaras, Elias
    [J]. JOURNAL OF FLUID MECHANICS, 2020, 884
  • [5] Flow Around a Comb Wing in Low-Reynolds-Number Flow
    Davidi, G.
    Weihs, D.
    [J]. AIAA JOURNAL, 2012, 50 (01) : 249 - 253
  • [6] DETERMINATION OF THE FLOW FIELD IN A REGION ADJACENT TO A STREAMLINED BODY AT SMALL REYNOLDS-NUMBER
    VASILEV, MM
    [J]. PMM JOURNAL OF APPLIED MATHEMATICS AND MECHANICS, 1977, 41 (06): : 1090 - 1096
  • [7] Low Reynolds Number Flow Around Tori of Different Slenderness
    Lazeroms, Werner M. J.
    de Tullio, Marco D.
    De Santis, Nicola
    Pizzoferrato, Roberto
    Verzicco, Roberto
    [J]. APPLIED SCIENCES-BASEL, 2017, 7 (11):
  • [8] Flow around a confined rotating cylinder at small Reynolds number
    Champmartin, Stephane
    Ambari, Abdelhak
    Roussel, Nicolas
    [J]. PHYSICS OF FLUIDS, 2007, 19 (10)
  • [9] On the effect of Reynolds number for flow around a row of square cylinders
    Sewatkar, C. M.
    Sharma, Atul
    Agrawal, Amit
    [J]. PHYSICS OF FLUIDS, 2009, 21 (08)
  • [10] Bifurcation Tracking for High Reynolds Number Flow Around an Airfoil
    Huntley, S.
    Jones, D.
    Gaitonde, A.
    [J]. INTERNATIONAL JOURNAL OF BIFURCATION AND CHAOS, 2017, 27 (04):