Performace of novel synthetic jet actuator under high ambient temperature
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摘要: 对高温环境下活塞式合成射流激励器的流场进行了数值模拟和试验研究,对比了激励器工作频率和射流孔直径,对常规、辅助进气激励器性能的影响。结果表明:在高温环境下,相对于常规进气,辅助进气可以显著地提高激励器性能,激励器吸气量、腔体峰值压比和射流峰值动量提高的同时,激励器出口截面射流峰值速度略有下降。辅助进气装置的效能最大区域为高工作频率或者小射流孔直径。相对于常规激励器,辅助进气激励器的吸气量、腔体峰值压比和射流峰值动量的增加幅度最大,分别增加了常规激励器的23073%、10397%和10737%(工作频率为250 Hz,射流孔直径为2 mm)。Abstract: The flow field of the piston-type synthetic jet actuator (SJA) under high ambient temperature was investigated numerically and experimentally. The effects of the actuation frequency and orifice diameter on conventional SJA and novel SJA were analyzed. The results indicated that the auxiliary air inlet can significantly increase the SJA performance under high ambient temperature. Compared with the conventional SJA, the novel SJA can increase the inlet mass flow rate, peak cylinder pressure ratio and peak jet momentum, despite of a little decrease of the peak jet velocity. The peak efficiency of the auxiliary air inlet lied in high actuation frequencies or small orifice diameter. Compared with the conventional SJA, the inlet mass flow rate, peak cylinder pressure ratio and peak jet momentum of novel SJA increased up to 23073%, 10397%, and 10737%, respectively, of conventional SJA at actuation frequency of 250 Hz, orifice diameter of 2 mm.
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Key words:
- synthetic jet /
- auxiliary air inlet /
- piston-type /
- actuator performance /
- cylinder pressure
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[1] 陈萍萍,乔渭阳,侯伟涛,等.基于流动控制技术的低稠度大负荷涡轮设计[J].航空动力学报,2010,25(11):2528-2537. CHEN Pingping,QIAO Weiyang,HOU Weitao,et al.Study on high-loading turbine airfoil design based on flow control[J].Journal of Aerospace Power,2010,25(11):2528-2537.(in Chinese) [2] 张宇超,谭慧俊,程林,等.低气压条件下多缝式等离子体合成射流激励器特性实验[J].航空动力学报,2018,33(3):711-716. ZHANG Yuchao,TAN Huijun,CHENG Lin,et al.Experiment on characteristics of plasma synthetic jet actuator with multiple slots under low pressure condition[J].Journal of Aerospace Power,2018,33(3):711-716.(in Chinese) [3] 谢永慧,屈焕成,何海宇.流动参数对合成射流控制叶栅流动分离的影响[J].航空动力学报,2013,28(3):636-645. XIE Yonghui,QU Huancheng,HE Haiyu.Influence of flow parameters on flow separation control of cascade with synthetic jet[J].Journal of Aerospace Power,2013,28(3):636-645.(in Chinese) [4] 秦勇,宋彦萍,陈浮,等.局部及全叶高合成射流对高速压气机静叶栅流场结构的影响[J].航空动力学报,2018,33(5):1204-1214. QIN Yong,SONG Yanping,CHEN Fu,et al.Influence of part-span and full-span synthetic jets on the flow structures within a high-speed compressor stator[J].Journal of Aerospace Power,2018,33(5):1204-1214.(in Chinese) [5] 魏佐君,段文华,乔渭阳,等.涡轮转子叶尖泄漏涡涡核稳定性及控制[J].航空动力学报,2018,33(9):2139-2149. WEI Zuojun,DUAN Wenhua,QIAO Weiyang,et al.Analysis and control of tio-leakage vortex core stability of turbine rotor[J].Journal of Aerospace Power,2018,33(9):2139-2149.(in Chinese) [6] 王林,罗振兵,夏智勋,等.合成双射流控制翼型分离流动的数值研究[J].空气动力学学报,2012,30(3):353-357. WANG Lin,LUO Zhenbing,XIA Zhixun,et al.Numerical simulation of separated flow control on an airfoil using dual synthetic jets[J].Acta Aerodynamic Sinica,2012,30(3):353-357.(in Chinese) [7] 李玉杰,罗振兵,邓雄,等.合成双射流控制NACA0015翼型大迎角流动分离试验研究[J].航空学报,2016,37(3):817-825. LI Yujie,LUO Zhenbing,DENG Xiong,et al.Experimental investigation on flow separation control of stalled NACA0015 airfoil using dual synthetic jet actuator[J].Acta Aeronautica et Astronautica Sinica,2016,37(3):817-825.(in Chinese) [8] XIA Zhixun,LUO Zhenbing.Physical factors of a primary jet vectoring using synthetic jet actuators[J].Applied Mathematics and Mechanics,2007,28(8):907-919. [9] LUO Zhenbing,XIA Zhixun,XIE Yonggao.Jet vectoring control using a novel synthetic jet actuator[J].Chinese Journal of Aeronautics,2007,20(3):193-201. [10] 王俊伟,夏智勋,罗振兵,等.合成射流对高超声速进气道启动特性影响数值模拟研究[J].空气动力学学报,2018,36(4):613-619. WANG Junwei,XIA Zhixun,LUO Zhenbing,et al.Numerical study on starting characteristics of hypersonic inlet with synthetic jet[J].Acta Aerodynamic Sinica,2018,36(4):613-619.(in Chinese) [11] Eriqitai,HONG Liang,LI Ting,et al.Effect of ambient temperature on piston-type synthetic jet actuator[J].SAGE-Journal of Aerospace Engineering,2017,232(6):1077-1086. [12] LUO Zhenbing,DENG Xia,XIA Zhixun,et al.Flow field and heat transfer characteristics of impingement based on a vectoring dual synthetic jet actuator[J].International Journal of Heat and Mass Transfer,2016,102(3):18-25. [13] 李彬彬.合成射流及在主动流动控制中的应用[D].南京:南京航空航天大学,2012. LI Binbin.Synthetic jets and its application in active flow control[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese) [14] SMITH B L.Synthetic jets and their interaction with adjacent jets[D].Atlanta,US:Georgia Institute of Technology,1999. [15] MALLINSON S G,REIZES J A,GUAN H.The operation and application of synthetic jet actuators[R].AIAA-2000-2402,2000. [16] DUANE C M,STEVEN A L,DOUGLAS G M,et al.Compact high-power boundary layer separation control actuator development[C]∥ASME Fluids Engineering Division Summer Meeting.New Orleans,US:ASME,2001:1-8. [17] GILARRANZ J L,YUE X,REDINIOTIS O K.PIV measurements and modeling of synthetic jet actuators for flow control[R].Washington DC:ASME Fluids Engineering Division Summer Meeting,1998. [18] SAMIMY M,KIM J,KASTNER J.Active control of high-speed and high Reynolds number jets using plasma actuators[J].Journal of Fluid Mechanics,2007,578(3):305-330. [19] 吴云,李应红.等离子体流动控制研究进展与展望[J].航空学报,2015,36(2):381-405. WU Yun,LI Yinghong.Progress andoutlook of plasma flow control[J].Acta Aeronautica et Astronautica Sinica,2015,36(2):381-405.(in Chinese) [20] 吕元伟.火花型合成射流对二元双喉道矢量喷管的流体主动控制研究[D].南京:南京航空航天大学,2016. Lv Yuanwei.Active flow control of dual-throat fluidic thrust-vectoring nozzle using synthetic jet driven by spark discharge[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2016.(in Chinese) [21] 刘欣,姜楠.喷口加齿湍射流增强混合的实验与数值研究[J].航空动力学报,2006,21(5):884-890. LIU Xin,JIANG Nan.Experimental and numerical study of jet mixing enhancement with wedged nozzle[J].Journal of Aerospace Power,2006,21(5):884-890.(in Chinese) [22] 李经警,张勃,吉洪湖.基于大涡模拟的圆转矩喷管尾喷流强化掺混机理研究[J].航空发动机,2018,44(2):27-34. LI Jingjing,ZHANG Bo,JI Honghu.Investigation on mixing enhancement mechanism of tail jet flow of circle-rectangular transition nozzle based on large eddy simulation[J].Aeroengine,2018,44(2):27-34.(in Chinese) [23] 聂萌萌,张靖周,谭晓茗.自耦合射流激励同向气流掺混的数值研究[J].航空动力学报,2009,24(12):2678-2682. NIE Mengmeng,ZHANG Jingzhou,TAN Xiaoming.Numerical investigation on two parallel flows mixing excited by synthetic jets[J].Journal of Aerospace Power,2009,24(12):2678-2682.(in Chinese) [24] PAREKH D E,KIBENS V,GLEZER A,et al.Innovative jet flow control:mixing enhancement experiments[R].AIAA 96-0308,1996. [25] DAVIS S A,GLEZER A.The manipulation of large- and small-scales in coaxial jets using synthetic jet actuators[R].AIAA-2000-0403,2000. [26] RITCHIE B D,MUJUMDAR D R,SEITZMAN J M.Mixing in coaxial jets using synthetic jet actuators[R].AIAA-2000-0404,2000. [27] CHEN Y,LIANG S,AUNG K.Enhanced mixing in a simulated combustor using synthetic jet actuators[R].AIAA 99-0449,1999. [28] WANG H,MENON S.Fuel-air mixing enhancement by synthetic micro jets[J].AIAA Journal,2001,39(12):2308-2319. [29] 罗振兵,夏智勋,胡建新,等.合成射流激励器增强同向燃气氧气掺混数值模拟及机理研究[J].固体火箭技术,2004,27(4):267-271. LUO Zhenbing,XIA Zhixun,HU Jianxin,et al.Numerical simulation and mechanism investigation on equidirectional fuel-air/oxygen mixing enhanced by synthetic jet actuators[J].Journal of Solid Rocket Technology,2004,27(4):267-271.(in Chinese) [30] 王猛杰.激波矢量控制和喷流强化混合的主次流干扰研究[D].北京:北京航空航天大学,2015. WANG Mengjie.A study of primary and secondary flow interaction of shock vector control and jet mixing enhancement[D].Beijing:Beijing University of Aeronautics and Astronautics,2015.(in Chinese) [31] Eerqitai,HONG Liang,LI Ting.A novel piston-type synthetic jet actuator with auxiliary air inlet[J].ASCE-Journal of Aerospace Engineering,2019,32(1):04018127.1-04018127.10.
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