瓣高宽比对波瓣强迫混合排气系统性能影响
Effect of ratio of height to width of lobe on the performance of a lobed mixer in a forced mixing exhaust system
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摘要: 以某涡扇发动机波瓣强迫混合排气系统为研究对象,在波瓣数以及波瓣长度不变的情况下,分别固定波瓣宽度改变波瓣高度和固定波瓣高度改变波瓣宽度,得到了一系列不同波瓣高宽比的几何模型,并对其进行了三维数值模拟研究,获得了不同高宽比对波瓣混合器流场、热混合效率和总压恢复系数的影响规律.结果表明:在混合器出口处,当高宽比在2~5范围内变化时,热混合效率在波瓣宽度和高度分别不变时,随高宽比的增加,分别呈现出不断增大以及不断减小的趋势;当宽度不变时,总压恢复系数随高宽比的增大而减小,当高度不变时,总压恢复系数随高宽比的增大而增大.Abstract: Geometric and numerical simulation models of lobed mixer with variation of the ratio of height to width (h/b) of lobe were created based on a lobed mixer in the forced mixing exhaust system of turbofan engine with constant lobe number and lobe length.Though three-dimensional numerical simulation,the principle of the effect of different ratios of height to width in a forced mixing exhaust system was obtained.The results show that at the exit section of the force mixing exhaust system,when the width of lobe is constant,the thermal mixing efficiency rises as h/b increases;however,when the height of lobe is constant,the mixing efficiency declines with rise of h/b.Besides,as h/b augments,the total-pressure recovery coefficient decreases if the width of lobe is unchanged,or increases if the height of lobe is invariable.
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Key words:
- forced mixing exhaust system /
- lobed mixer /
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[1] Presz W M,Reynolds G,Mccormick,D C.Thrust augment using mixer-ejector-diffuser systems .AIAA Paper 94-0020,1994. [2] Presz W M.Mixer/ejector noise suppressors .AIAA Paper 91-2243,1991. [3] 张靖周,李立国,高潮,等.波瓣喷管红外抑制系统的实验 研究[J].航空动力学报,1997,12(2):212-214. ZHANG Jingzhou,LI Liguo,GAO Chao,et al.An experimental study on a lobed nozzle of an infrared suppression system[J].Journal of Aerospace Power,1997,12(2):212-214.(in Chinese) [4] 刘友宏,陈锵,李立国.圆排波瓣圆柱混合管的气动特性实验研究[J].南京航空航天大学学报,2000,32(4):375-380. LIU Youhong,CHEN Qiang,LI Liguo.Experimental investigation of internal aerodynamics of periodically axi-symmetry lobed exhaust-ejector mixers[J].Journal of Nanjing Univesity of Aeronautics & Astronautics,2000,32(4):375-380.(in Chinese) [5] 刘友宏,李立国.有无中心锥圆排波瓣喷管引射器内流场模拟与比较[J].航空动力学报,2002,17(3):280-286. LIU Youhong,LI Liguo.Numerical simulation of flow field in circularly lobed exhaust-ejector mixer with/without a central plug[J].Journal of Aerospace Power,2002,17(3):280-286.(in Chinese) [6] LIU Youhong.Experimental and numerical research on high pumping performance mechanism of lobed exhauster-ejector[J].International Communication of Heat and Mass Transfer,2007,34(2):197-209. [7] LIU Youhong.Experimental and numerical investigation of circularly lobed ejector with bend mixer[J].Heat Transfer-Asian Research,2007,36(7):387-397. [8] Waitz I A,Qiu Y J,Manning T A,et al.Enhanced mixing with streamwise vorticity [J].Progress in Aerospace Sciences,1997,33(5-6):323-351. [9] Cooper N J,Merati P,HU Hui.Numerical simulation of the vortical structures in a lobed jet mixing flow .AIAA 2005-635,2005. [10] Skebe S A,Paterson R W,Barber T J.Experimental investigation of three-dimensional forced mixer lobed flow fields .AIAA Paper 88-3785,1988. [11] 刘友宏,谢翌.菊花形混合器混合效率理论计算[J].航空动力学报,2009,24(4):740-745. LIU Youhong,XIE Yi.Analytical solution of mixing efficiency of lobed mixer[J].Journal of Aerospace Power,2009,24(4):740-745.(in Chinese) [12] Frost T H.Practical bypass mixing systems for fan jet aero-engines[J].Aeronautical Quarterly,1966,17:141-160. [13] 郭楠.菊花形混合器流场计算与设计优化 .北京:北京航空航天大学,2008. GUO Nan.Numerical simulation of the flow field and the optimal design of lobed mixer .Beijing:Beijing University of Aeronautics and Astronautics,2008.(in Chinese) -
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