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BALLISIIC AND AIRDYNAMICS

Numerical Simulationof Drag Reduction of Dimple Surface with Different Spacing in Air

  • PENG Shichong ,
  • DONG Yanfei ,
  • YIN Xiaohui
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  • School of Aircraft Engineering, Nanchang Hangkong University, Nanchang 330063, China

Received date: 2012-12-07

  Online published: 2025-05-26

Abstract

Currently, bionic non-smooth surface drag reduction technology with significant economic value and military value is still imperfect. Generally, dimple structure, flow velocity, fluid medium and other factors are related to the dimple surface drag reduction. In order to further analyze the pit surface drag reduction, the numerical simulation was carried on the flowing of dimple non-smooth surface with different spacing in air. The results show that this kind of unsmooth surface with dimples (r = 0.5s, h = 0.25mm, a = 5mm) has a good local optimum drag reduction effect on flow velocity ranging from 6m/s to 15m/s, and it has the best reducing ability (25.927%) at the velocity of 6m/s. Finally, the theory of the drag reduction and the impact of the dimples drag reduction factors (different spacing) were analyzed. Interval length relative to the concave surface size has an appropriate value.

Cite this article

PENG Shichong , DONG Yanfei , YIN Xiaohui . Numerical Simulationof Drag Reduction of Dimple Surface with Different Spacing in Air[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(5) : 133 -137,140 . DOI: 10.15892/j.cnki.djzdxb.2013.05.006

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References

[1]
Bechert D W,Bruse M,Hage W,et al. Fluid mechanics of biological surfaces and their technological application[J]. Naturwissenschaften,2000, 87(4): 157-171.
[2]
Hermann Lienhart,Michael Breuer,Cagatay Koksoy. Drag reduction by dimples: A complementary experimental /numerical investigation [J]. International Journal of Heat and Fluid Flow,2008,29(3): 783-791.
[3]
杨弘伟,高歌.一种新型边界层控制技术应用于湍流减阻的实验研究[J].航空学报, 1997,18(4): 455-457.
[4]
赵军.凹坑形仿生非光滑表面的减阻性能研究[D].大连: 大连理工大学, 2008.
[5]
刘占一,胡海豹,宋保维,等.不同间隔脊状表面的减阻数值仿真研究[J].系统仿真学报,2009,21 (19): 6025-6028.
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