超声速湍流边界层阵列式微吹气流动控制与减阻特性

doi:10.7527/S1000-6893.2023.29396

Abstract

Abstract:

Direct Numerical Simulations （DNS） are used to study the flow control mechanism and drag reduction characteristics of square micropores array micro-blowing on supersonic turbulent boundary layer. The 0.3 mm × 0.3 mm micropores array with a horizontal and longitudinal number of 88×6 is arranged in the spatially developing turbulent region. The horizontal and longitudinal center distance of porous region is 0.6 mm， and the porosity is 25%. The amplitudes of micro-blowing array are 0.2% （B1）， 0.4% （B2） and 0.6% （B3） of the freestream velocity， respectively. The calculation results show that the micro-blowing technology can reduce surface friction on supersonic turbulent boundary layer. The total friction of porous region is reduced by 23% at the blowing amplitude of 0.6%， and the drag reduction rate approximately exhibits a linear increase with the increase of micro-blowing amplitude. The results of the turbulent kinetic energy equilibrium analysis show that all source terms of the turbulent kinetic energy equilibrium equation are enhanced after blowing control is applied. The micro-blowing technology promotes the energy cascade process in the near-wall region， and destroys the self-sustaining mechanism between velocity streaks and quasi-streamwise vortices within the original turbulent boundary layer. The quadrant analysis of velocity pulsation on boundary layer shows that the drag reduction of the micro-blowing technique comes from its inhibitory effect on the downward sweeping process in the near-wall region.

Key words: micro-blowing, square micropores array, turbulent boundary layer, drag reduction, turbulent coherent structure

CLC Number:

V211.3

Fanyu ZENG, Yunlong QIU, Zhanwei CAO, Lun ZHANG, Weifang CHEN. Flow control and drag reduction characteristics of micro-blowing array on supersonic turbulent boundary layer[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729396-729396.

Figures/Tables 15

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References 37

1	RICCO P， SKOTE M， LESCHZINER M A. A review of turbulent skin-friction drag reduction by near-wall transverse forcing［DB/OL］. arXiv preprint： 2103.04719， 2021
2	KORNILOV V. Current state and prospects of researches on the control of turbulent boundary layer by air blowing［J］. Progress in Aerospace Sciences， 2015， 76： 1-23.
3	CORKE THOMAS C， THOMAS FLINT O. Active and passive turbulent boundary-layer drag reduction［J］. AIAA Journal， 2018， 56（10）： 3835-3847.
4	WALSH M J. Riblets as a viscous drag reduction technique［J］. AIAA Journal， 2012， 21（4）： 485-486.
5	LI W P. Turbulence statistics of flow over a drag-reducing and a drag-increasing riblet-mounted surface［J］. Aerospace Science and Technology， 2020， 104： 106003.
6	WANG L H， HUANG W X， XU C X， et al. Relationship between wall shear stresses and streamwise vortices［J］. Applied Mathematics and Mechanics， 2019， 40（3）： 381-396.
7	FUKAGATA K， KERN S， CHATELAIN P， et al. Evolutionary optimization of an anisotropic compliant surface for turbulent friction drag reduction［J］. Journal of Turbulence， 2008， 9： N35.
8	YAO J E， CHEN X， HUSSAIN F. Drag control in wall-bounded turbulent flows via spanwise opposed wall-jet forcing［J］. Journal of Fluid Mechanics， 2018， 852： 678-709.
9	CHENG X Q， WONG C W， HUSSAIN F， et al. Flat plate drag reduction using plasma-generated streamwise vortices［J］. Journal of Fluid Mechanics， 2021， 918： A24.
10	白建侠，姜楠，唐湛棋，等. 双压电振子异步振动主动调制湍流边界层流向涡减阻［J］. 航空动力学报， 2019， 34（12）： 2539-2548.
	BAI J X， JIANG N， TANG Z Q， et al. Active modulation to streamwise vortex drag reduction of turbulent boundary layer by asynchronous vibration with double piezoelectric vibrator［J］. Journal of Aerospace Power， 2019， 34（12）： 2539-2548 （in Chinese）.
11	JI S C， ZHANG B， LI J A， et al. Numerical study for active flow control using dielectric barrier discharge actuators［J］. Journal of Aerospace Engineering， 2017， 30（5）： 04017050.
12	KAMETANI Y， FUKAGATA K. Direct numerical simulation of spatially developing turbulent boundary layers with uniform blowing or suction［J］. Journal of Fluid Mechanics， 2011， 681： 154-172.
13	MA R， GAO Z H， LU L S， et al. Skin-friction drag reduction by local porous uniform blowing in spatially developing compressible turbulent boundary layers［J］. Physics of Fluids， 2022， 34： 125130.
14	LIU Q A， LUO Z B， WANG L， et al. Direct numerical simulations of supersonic turbulent boundary layer with streamwise-striped wall blowing［J］. Aerospace Science and Technology， 2021， 110： 106510.
15	KAMETANI Y， FUKAGATA K， ÖRLÜ R， et al. Drag reduction in spatially developing turbulent boundary layers by spatially intermittent blowing at constant mass-flux［J］. Journal of Turbulence， 2016， 17（10）： 913-929.
16	Kim K， Sung H J. DNS of turbulent boundary layer with time-periodic blowing through a spanwise slot［C］∥Proceedings of the Asian Computational Fluid Dynamics Conference （5th）. Busan， 2003： 835-842.
17	KIM K， SUNG H J. Effects of periodic blowing from spanwise slot on a turbulent boundary layer［J］. AIAA Journal， 2003， 41（10）： 1916-1924.
18	KIM K， JIN SUNG H. Effects of unsteady blowing through a spanwise slot on a turbulent boundary layer［J］. Journal of Fluid Mechanics， 2006， 557： 423.
19	CHENG X Q， QIAO Z X， ZHANG X， et al. Skin-friction reduction using periodic blowing through streamwise slits［J］. Journal of Fluid Mechanics， 2021， 920： A50.
20	ZHANG X， WONG C W， CHENG X Q， et al. Dependence of skin-friction reduction on the geometric parameters of blowing jet array［J］. Physics of Fluids， 2022， 34（10）： 105125.
21	HWANG D， BIESIADNY T. Experimental evaluation of penalty associated with micro-blowing for reducing skin friction［C］∥Proceedings of the 36th AIAA Aerospace Sciences Meeting and Exhibit. Reston： AIAA， 1998： AIAA1998-677.
22	HWANG D. Review of research into the concept of the microblowing technique for turbulent skin friction reduction［J］. Progress in Aerospace Sciences， 2005， 40（8）： 559-575.
23	HWANG D. An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique［C］∥Proceedings of the 38th Aerospace Sciences Meeting and Exhibit. Reston： AIAA， 2000： AIAA2000-545.
24	KORNILOV V I， BOIKO A V. Efficiency of air microblowing through microperforated wall for flat plate drag reduction［J］. AIAA Journal， 2012， 50（3）： 724-732.
25	范云涛，张阳，叶志贤，等. 微吹气对湍流平板边界层流动特性的影响及其减阻机理［J］. 航空学报， 2020， 41（10）： 123814.
	FAN Y T， ZHANG Y， YE Z X， et al. Micro-blowing： Effect on flow characteristics in turbulent flat plate boundary layer and drag reduction mechanism［J］. Acta Aeronautica et Astronautica Sinica， 2020， 41（10）： 123814 （in Chinese）.
26	PIROZZOLI S， GRASSO F， GATSKI T B. Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25［J］. Physics of Fluids， 2004， 16（3）： 530-545.
27	LI X L， FU D X， MA Y W， et al. Acoustic calculation for supersonic turbulent boundary layer flow［J］. Chinese Physics Letters， 2009， 26（9）： 094701.
28	傅德薰，马延文，李新亮. 可压缩湍流直接数值模拟［M］. 北京：科学出版社， 2010.
	FU D X， MA Y W， LI X L. Direct numerical simulation of compressible turbulence［M］. Beijing： Science Press， 2010 （in Chinese）.
29	WHITE F M. Viscous fluid flow［M］. New York： McGraw-Hill， 1974.
30	WU X H， MOIN P. Transitional and turbulent boundary layer with heat transfer［J］. Physics of Fluids， 2010， 22（8）： 085105.
31	Spalart P R. Direct simulation of a turbulent boundary layer up to Re_θ =1410［J］. Journal Fluid Mechanics， 1988， 187： 61.
32	KAMETANI Y， KOTAKE A， FUKAGATA K， et al. Drag reduction capability of uniform blowing in supersonic wall-bounded turbulent flows［J］. Physical Review Fluids， 2017， 2（12）： 123904.
33	CHOI H， MOIN P， KIM J. Active turbulence control for drag reduction in wall-bounded flows［J］. Journal of Fluid Mechanics， 1994， 262： 75-110.
34	XU C X， DENG B Q， HUANG W X， et al. Coherent structures in wall turbulence and mechanism for drag reduction control［J］. Science China Physics， Mechanics and Astronomy， 2013， 56（6）： 1053-1061.
35	XU C. Coherent structures and drag-reduction mechanism in wall turbulence［J］. Advances in Mechanics， 2015， 45： 111-140.
36	JIMÉNEZ J， PINELLI A. The autonomous cycle of near-wall turbulence［J］. Journal of Fluid Mechanics， 1999， 389： 335-359.
37	LI W P， FAN Y T， MODESTI D， et al. Decomposition of the mean skin-friction drag in compressible turbulent channel flows［J］. Journal of Fluid Mechanics， 2019， 875： 101-123.

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Flow control and drag reduction characteristics of micro-blowing array on supersonic turbulent boundary layer

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