横向射流条件下超燃冲压发动机燃料喷注雾化综述
详细信息 查看官网全文
- 论文作者：孛涛 ; 李娜 ; 王伟良 ; 魏祥庚 ; 秦飞
- 年：2016
- 作者机构：西北工业大学;
- 论文关键词：超音速燃烧 ; 横向射流 ; 燃料雾化 ; 穿透深度
- 会议召开时间：2016-08-17
- 会议录名称：中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议论文集
- 语种：中文
- 分类号：V235.21
- 学会代码：HTDZ
- 会议名称：中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议
- 会议地点：中国陕西西安
- 主办单位：中国航天第三专业信息网、中国航天科技集团公司科技委、中国航天科工集团公司科技委
- 学会名称：中国航天第三专业信息网
- 页数：9
- 文件大小：1430k
- 原文格式：D
- 会议级别：全国
摘要
超燃冲压发动机与高超声速飞行的实现密切相关,有着广阔的运用前景。与传统的液体火箭发动机不同,组织燃烧需要从环境中摄取氧化剂,因此受到工作条件,工作性质,总体物理性能等多方面的制约。对于超音速状态下燃烧,燃料以适当的方式进行喷注雾化、与主流的掺混是发动机正常工作首先要解决的问题。针对超燃条件下高马赫数的客观情况,本文首先介绍了横向射流条件下的燃料喷注原理,而后着重介绍了燃料的雾化机理以及在此射流条件下燃料喷注的实现、喷注位置以及喷注穿透深度的研究现状并提出了以后的研究思路与方向。
引文
[1]Ferri,A.Mixing-Controlled Supersonic combustion[J].Anna.Rev.Fluid.Mech.,1973,5:301-338.
[2]徐朝启.宽适用性RBCC燃烧室燃烧组织技术研究[D].西安:西北工业大学博士学位论文,2014.
[3]张漫.RBCC燃烧室湍流喷雾燃烧及其稳定机制研究[D].西安:西北工业大学博士学位论文,2010.
[4]耿辉.超声速燃烧室中凹腔上游横向喷注燃料的流动、混合与燃烧特性研究[D].长沙:国防科学技术大学博士学位论文,2007.
[5]Adela Ben-Yakar.Experimental investigation of mixing and ignition of transverse jets in supersonic crossflows[D].Ph D’s Dissertation,Stanford University,2000.
[6]A.Ben-yakar,M.Kamel,C.Morris,et al.Experimental investigation of H2 transverse jet combustion in hypervelocity flows[J].AIAA Paper,97-3019.
[7]刘君.超声速完全气体和非平衡气体的复杂喷流流场数值模拟[D].中国空气动力研究与发展中心研究生部博士学位论文,1993.
[8]杨彦广,章起华,刘君高.超声速主流中完全气体横向喷流干扰特性研究[J].空气动力学学报,2005,23(3):299-306.
[9]赵桂林,彭辉,胡亮等.超声速流动中侧向喷流干扰特性的实验研究[J].力学学报,2004,36(5):577-582
[10]王军旗,李素循.平板超声速湍流喷流干扰流场特性[C].全国第十三届高超声速气动力热学术交流会议论文集:338-342
[11]Schetz,J.A.Injection and mixing in turbulent flow[C].In vol.68 of Progress in Aeronautics and Astronautics,AIAA.1980.
[12]Chigier,N.and Reitz,R.D.Regimes of break-up and breakup mechanisms(physical aspects)in Recent Advances in Spray Combustion:Spray Atomization and Drop Burning Phenomena(K.K.Kuo,Ed.)[C].Vol.166 of Progress in Aeronautics and Astronautics,AIAA,pp.159-222,1996.
[13]翟振辰,周进,韩旭.超声速流场中横向燃料射流混合过程的实验研究[C].第十四届全国激波与激波管学术会议,2010.
[14]Portz R.,Segal C.Penetration of gaseous jets in supersonic flows[R].AIAA-2006-1229
[15]R.C.Orth,J.A.Funk.An experimental and comparative study of jet penetration in supersonic flow[J].Journal of Propulsion and Power,1967,4(9):1236-1242.
[16]F.S.Billing,R.C.Orth,M.Lasky.A unified analysis gaseous jet penetration[J].AIAA Journal,1971,9(6):1048-1058.
[17]D.Papamoschou,D.G.Hubbard.Visual observations of supersonic transverse jets[J].Experiments in Fluids,1993,14:468-475
[18]M.P.Lee,B.K.Mc Millin,J.L.Palmer,et al.Planar fluorescence imaging of a transverse jet in a supersonic crossflows[J].Journal of Propulsion and Powers,1992,8(4):729-735.
[19]王延胜,林宇震,李林.基于PLIF技术的航空煤油横向射流穿透深度研究[J].推进技术,Vol.36,No.9,2015.
[20]G.Yu,J.G.Li,J.R.Zhao,L.J.Yue,X.Y.C hang.An experimental study of kerosene combustion in a supersonic model combustor using excrescent atomization[J].Proceedings of the Combustion Institute 30(2005)2859–2866.
[21]李春.超声速气流中液体横向射流结构特性实验研究[D].长沙:国防科学技术大学博士学位论文,2013.
[22]张岩.超燃冲压发动机燃料喷注方案综述[J].推进技术,NO.2,2014
[23]Zhou Song-bai,Liu Jun,Guo Zheng,Wang Wei,Geng Hui.Numerical Simulation for the Fuel Jet and Inner Flow field of Scramjet Combustion Chamber(in Chinese)[J].Journal of National University of Defense Technology,Vol.29 No.2 2007.
[24]Fox J S,Gastont M J,et al.Instantaneous mole-fraction PLIF imaging of mixing layers behind hyper mixinginjectors[J].AIAA 1999-0774
[25]Cox S.K,Fuller R.P,Schetz J A,et al.Vertical Interactions Generated by an Injector Array to Enhance Mixing in Supersonic Flow[J].AIAA 1994-0708
[26]Livingston T,Segal C,Schindler M,et al.Penetration and Spreading of Liquid Jets in an External-Internal Compression Inlet[J].AIAA Journal,2000,38(6)
[27]黄冉.超燃冲压发动机燃烧室支板绕流及喷射流场大涡模拟[D].长沙:国防科学技术大学博士学位论文,2006.
[28]Cattafesta L N,Williams D,Rowley C,et al.Review of active control of flow-induced cavity oscillations[J].Progress in Aerospace Sciences,2008,44.
[29]Venkateswaran Narayanaswamy,Laxminarayan L Raja,Noel T.Clemens.Characterization of a high-frequency pulsed-plasmajet actuator for supersonic flow control[J].AIAA Journal,2010,48
[30]潘科玮,何国强,刘佩进.RBCC发动机燃料喷注位置变化对混合燃烧模式燃烧的影响[J].Journal of Aerospace Power,Vol.26 No.8,2011.
[31]万少文,何国强,刘佩进.RBCC混合燃烧模式下燃料喷注位置对燃烧性能影响研究[J].Journal of Solid Rocket Technology,Vol.33 No.6,2010.
[32]Vinogradov,V.A.and Prudnikov,A.G.Injection of liquid into the strut shadow at supersonic velocities[J].Society of Automotive Engineers.SAE-931455.
[33]Sabel’nikov,V.A.and Prezin,V.I.Scramjet research and development in Russia,in Scramjet Propulsion(E.T.Curran and S.N.B.Murthy,eds.),Vol.189 of Progress in Astronautics and Aeronautics,AIAA,pp.223-367,2000.
[34]Wang Liao,Zhang Cheng Liang.Experimental investigation of kerosene supersonic combustion test using aerated-liquid injectors[J].Journal of Aerospace Power,Vol.24 No.2,2009.
[35]Liu Jing,Xu xu.Application on numerical simulation of atomization of liquid jet in Crossflow using two atomization model[J].Journal of Aerospace Power,Vol.28 No.87,2013.
[36]Kolpin M A,Horn K P,Reichenbach R E.Study of penetration of a liquid inject ant into a supersonic flow[J].AIAA Journal,1968,6(5):8532858.
[37]Allan S,Joseph S.Breakup of liquid sheet s and jet s in a supersonic gas stream[J].AIAA Journal,1971,9(4):6662673.
[38]Kush E.A,J r,Schetz J A.Liquid jet injection into a supersonic flow[J].AIAA Journal,1973,11(9):122321224
[39]Schetz J.A,Kush E.A.J r,Joshi P B.Wave phenomena in liquid jet breakup in a supersonic Crossflow[J].AIAA Journal,1980,18(7):7742778
[40]Lin K C,Kennedy P J,Jackson T A.Structures of water jet s in a Mach 1.94 supersonic Crossflow[R].AIAA,2004,2971,2004.
[41]徐胜利,Archer R D,Milton B E,等.煤油在超声速气流中非定常横向喷射的实验观察[J].空气动力学学报,2000,18(3):2722279.
[42]刘静,徐旭.超声速横向气流中喷雾的数值模拟[J].火箭推进,Vol.32,No.5,2006.
[43]刘静,徐旭.超声速横向气流中燃料雾化的数值模拟[J].北京航空航天大学学报,Vol.36,No.10,2010.
[44]刘静,王辽,张佳.超声速气流中横向射流雾化实验和数值模拟[J].Journal of Aerospace Power,Vol.23 No.4,2008.
[45]Liu Jing,Xu Xu.Direct Numerical Simulation of Secondary Breakup of Liquid Drops[J].Chinese Journal of Aeronautics 23(2010)153-161
[46]仝毅恒.横向气流中液体射流喷注特性和破碎过程研究[D].长沙:国防科学技术大学博士学位论文,2012.
[47]王雄辉,黄勇,王方.横向气流中液体射流袋式破碎机理[J].推进技术,Vol.33,No.2,2012.
[48]王雄辉,黄勇,王方.横向气流中液体圆柱射流的破碎特性和表面波现象[J].Journal of Aerospace Power,Vol.27 No.9,2012.
[49]刘静,徐旭.两种雾化模型在横向流雾化数值模拟中的应用[J].Journal of Aerospace Power,Vol.28No.7,2013.
[50]刘静,徐旭.高速气流中横向液体射流雾化研究进展[J].力学进展,Vol.39 No.3,.
[51]Reitz R D,Diwakar R.Structure of high-pressure fuel sprays[C].SAE870598.
[52]Habchi C,Vehoeven D.Modeling atomization and breakup in high-pressure diesel sprays[C].SAE970881.
[53]Trinh H P,Chen C P.Modeling of turbulence effects on liquid jet atomization and breakup[J].AIAA-2005-0154.
[54]Kush,E.A.,Jr.and Schetz,J.A.Liquid jet injection into a supersonic flow[J].AIAA J.11,1223-1224.
[55]Povinelli,F.P.and Povinelli,R.J.Correlation of secondary sonic and supersonic gaseous jet penetration into supersonic crossflows[J].NASA TN D-6370.
[56]Mc Clinton,C.R.(1974).“Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream[J].NASA TM X-3030.
[57]Orth,R.C.,Schetz,J.A.,and Billig,F.S.The interaction and penetration of gaseous jet in supersonic crossflows[J]NASA CR-1386.
[58]Liscinsky,D.S.True,B.,and Holdeman,M.A.Crossflow mixing of noncircular jets[J].AIAA Paper 95-0732.
[59]Kolpin M A,Horn K P,Reichenbach R E.Study of penetrationof a liquid inject ant into a supersonic flow[J].AIAAJournal,6(5):853 858,1968.
[60]杨银军,窦志国,段立伟.超声速来流中横向喷流角度对流动与混合特性的影响[J].Modern Electronics Technique,Vol.36,No.17.
[61]Liu Jing,Numerical and experimental investigation of fuel spray in supersonic cross flow[D].北京:北京航空航天大学博士论文,2010.
[62]Corin Segal.The Scramjet Engine:Process and Characteristics[M].Cambridge University Press.ISBN 978-7-80243-954-2(2009)
[63]Jinho Lee,Kuo-Cheng Lin,Dean Eklund.Challenges in Fuel Injection for High-Speed Propulsion Systems[J].AIAA JOURNAL,Vol.53,No.6,2015.
[2]徐朝启.宽适用性RBCC燃烧室燃烧组织技术研究[D].西安:西北工业大学博士学位论文,2014.
[3]张漫.RBCC燃烧室湍流喷雾燃烧及其稳定机制研究[D].西安:西北工业大学博士学位论文,2010.
[4]耿辉.超声速燃烧室中凹腔上游横向喷注燃料的流动、混合与燃烧特性研究[D].长沙:国防科学技术大学博士学位论文,2007.
[5]Adela Ben-Yakar.Experimental investigation of mixing and ignition of transverse jets in supersonic crossflows[D].Ph D’s Dissertation,Stanford University,2000.
[6]A.Ben-yakar,M.Kamel,C.Morris,et al.Experimental investigation of H2 transverse jet combustion in hypervelocity flows[J].AIAA Paper,97-3019.
[7]刘君.超声速完全气体和非平衡气体的复杂喷流流场数值模拟[D].中国空气动力研究与发展中心研究生部博士学位论文,1993.
[8]杨彦广,章起华,刘君高.超声速主流中完全气体横向喷流干扰特性研究[J].空气动力学学报,2005,23(3):299-306.
[9]赵桂林,彭辉,胡亮等.超声速流动中侧向喷流干扰特性的实验研究[J].力学学报,2004,36(5):577-582
[10]王军旗,李素循.平板超声速湍流喷流干扰流场特性[C].全国第十三届高超声速气动力热学术交流会议论文集:338-342
[11]Schetz,J.A.Injection and mixing in turbulent flow[C].In vol.68 of Progress in Aeronautics and Astronautics,AIAA.1980.
[12]Chigier,N.and Reitz,R.D.Regimes of break-up and breakup mechanisms(physical aspects)in Recent Advances in Spray Combustion:Spray Atomization and Drop Burning Phenomena(K.K.Kuo,Ed.)[C].Vol.166 of Progress in Aeronautics and Astronautics,AIAA,pp.159-222,1996.
[13]翟振辰,周进,韩旭.超声速流场中横向燃料射流混合过程的实验研究[C].第十四届全国激波与激波管学术会议,2010.
[14]Portz R.,Segal C.Penetration of gaseous jets in supersonic flows[R].AIAA-2006-1229
[15]R.C.Orth,J.A.Funk.An experimental and comparative study of jet penetration in supersonic flow[J].Journal of Propulsion and Power,1967,4(9):1236-1242.
[16]F.S.Billing,R.C.Orth,M.Lasky.A unified analysis gaseous jet penetration[J].AIAA Journal,1971,9(6):1048-1058.
[17]D.Papamoschou,D.G.Hubbard.Visual observations of supersonic transverse jets[J].Experiments in Fluids,1993,14:468-475
[18]M.P.Lee,B.K.Mc Millin,J.L.Palmer,et al.Planar fluorescence imaging of a transverse jet in a supersonic crossflows[J].Journal of Propulsion and Powers,1992,8(4):729-735.
[19]王延胜,林宇震,李林.基于PLIF技术的航空煤油横向射流穿透深度研究[J].推进技术,Vol.36,No.9,2015.
[20]G.Yu,J.G.Li,J.R.Zhao,L.J.Yue,X.Y.C hang.An experimental study of kerosene combustion in a supersonic model combustor using excrescent atomization[J].Proceedings of the Combustion Institute 30(2005)2859–2866.
[21]李春.超声速气流中液体横向射流结构特性实验研究[D].长沙:国防科学技术大学博士学位论文,2013.
[22]张岩.超燃冲压发动机燃料喷注方案综述[J].推进技术,NO.2,2014
[23]Zhou Song-bai,Liu Jun,Guo Zheng,Wang Wei,Geng Hui.Numerical Simulation for the Fuel Jet and Inner Flow field of Scramjet Combustion Chamber(in Chinese)[J].Journal of National University of Defense Technology,Vol.29 No.2 2007.
[24]Fox J S,Gastont M J,et al.Instantaneous mole-fraction PLIF imaging of mixing layers behind hyper mixinginjectors[J].AIAA 1999-0774
[25]Cox S.K,Fuller R.P,Schetz J A,et al.Vertical Interactions Generated by an Injector Array to Enhance Mixing in Supersonic Flow[J].AIAA 1994-0708
[26]Livingston T,Segal C,Schindler M,et al.Penetration and Spreading of Liquid Jets in an External-Internal Compression Inlet[J].AIAA Journal,2000,38(6)
[27]黄冉.超燃冲压发动机燃烧室支板绕流及喷射流场大涡模拟[D].长沙:国防科学技术大学博士学位论文,2006.
[28]Cattafesta L N,Williams D,Rowley C,et al.Review of active control of flow-induced cavity oscillations[J].Progress in Aerospace Sciences,2008,44.
[29]Venkateswaran Narayanaswamy,Laxminarayan L Raja,Noel T.Clemens.Characterization of a high-frequency pulsed-plasmajet actuator for supersonic flow control[J].AIAA Journal,2010,48
[30]潘科玮,何国强,刘佩进.RBCC发动机燃料喷注位置变化对混合燃烧模式燃烧的影响[J].Journal of Aerospace Power,Vol.26 No.8,2011.
[31]万少文,何国强,刘佩进.RBCC混合燃烧模式下燃料喷注位置对燃烧性能影响研究[J].Journal of Solid Rocket Technology,Vol.33 No.6,2010.
[32]Vinogradov,V.A.and Prudnikov,A.G.Injection of liquid into the strut shadow at supersonic velocities[J].Society of Automotive Engineers.SAE-931455.
[33]Sabel’nikov,V.A.and Prezin,V.I.Scramjet research and development in Russia,in Scramjet Propulsion(E.T.Curran and S.N.B.Murthy,eds.),Vol.189 of Progress in Astronautics and Aeronautics,AIAA,pp.223-367,2000.
[34]Wang Liao,Zhang Cheng Liang.Experimental investigation of kerosene supersonic combustion test using aerated-liquid injectors[J].Journal of Aerospace Power,Vol.24 No.2,2009.
[35]Liu Jing,Xu xu.Application on numerical simulation of atomization of liquid jet in Crossflow using two atomization model[J].Journal of Aerospace Power,Vol.28 No.87,2013.
[36]Kolpin M A,Horn K P,Reichenbach R E.Study of penetration of a liquid inject ant into a supersonic flow[J].AIAA Journal,1968,6(5):8532858.
[37]Allan S,Joseph S.Breakup of liquid sheet s and jet s in a supersonic gas stream[J].AIAA Journal,1971,9(4):6662673.
[38]Kush E.A,J r,Schetz J A.Liquid jet injection into a supersonic flow[J].AIAA Journal,1973,11(9):122321224
[39]Schetz J.A,Kush E.A.J r,Joshi P B.Wave phenomena in liquid jet breakup in a supersonic Crossflow[J].AIAA Journal,1980,18(7):7742778
[40]Lin K C,Kennedy P J,Jackson T A.Structures of water jet s in a Mach 1.94 supersonic Crossflow[R].AIAA,2004,2971,2004.
[41]徐胜利,Archer R D,Milton B E,等.煤油在超声速气流中非定常横向喷射的实验观察[J].空气动力学学报,2000,18(3):2722279.
[42]刘静,徐旭.超声速横向气流中喷雾的数值模拟[J].火箭推进,Vol.32,No.5,2006.
[43]刘静,徐旭.超声速横向气流中燃料雾化的数值模拟[J].北京航空航天大学学报,Vol.36,No.10,2010.
[44]刘静,王辽,张佳.超声速气流中横向射流雾化实验和数值模拟[J].Journal of Aerospace Power,Vol.23 No.4,2008.
[45]Liu Jing,Xu Xu.Direct Numerical Simulation of Secondary Breakup of Liquid Drops[J].Chinese Journal of Aeronautics 23(2010)153-161
[46]仝毅恒.横向气流中液体射流喷注特性和破碎过程研究[D].长沙:国防科学技术大学博士学位论文,2012.
[47]王雄辉,黄勇,王方.横向气流中液体射流袋式破碎机理[J].推进技术,Vol.33,No.2,2012.
[48]王雄辉,黄勇,王方.横向气流中液体圆柱射流的破碎特性和表面波现象[J].Journal of Aerospace Power,Vol.27 No.9,2012.
[49]刘静,徐旭.两种雾化模型在横向流雾化数值模拟中的应用[J].Journal of Aerospace Power,Vol.28No.7,2013.
[50]刘静,徐旭.高速气流中横向液体射流雾化研究进展[J].力学进展,Vol.39 No.3,.
[51]Reitz R D,Diwakar R.Structure of high-pressure fuel sprays[C].SAE870598.
[52]Habchi C,Vehoeven D.Modeling atomization and breakup in high-pressure diesel sprays[C].SAE970881.
[53]Trinh H P,Chen C P.Modeling of turbulence effects on liquid jet atomization and breakup[J].AIAA-2005-0154.
[54]Kush,E.A.,Jr.and Schetz,J.A.Liquid jet injection into a supersonic flow[J].AIAA J.11,1223-1224.
[55]Povinelli,F.P.and Povinelli,R.J.Correlation of secondary sonic and supersonic gaseous jet penetration into supersonic crossflows[J].NASA TN D-6370.
[56]Mc Clinton,C.R.(1974).“Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream[J].NASA TM X-3030.
[57]Orth,R.C.,Schetz,J.A.,and Billig,F.S.The interaction and penetration of gaseous jet in supersonic crossflows[J]NASA CR-1386.
[58]Liscinsky,D.S.True,B.,and Holdeman,M.A.Crossflow mixing of noncircular jets[J].AIAA Paper 95-0732.
[59]Kolpin M A,Horn K P,Reichenbach R E.Study of penetrationof a liquid inject ant into a supersonic flow[J].AIAAJournal,6(5):853 858,1968.
[60]杨银军,窦志国,段立伟.超声速来流中横向喷流角度对流动与混合特性的影响[J].Modern Electronics Technique,Vol.36,No.17.
[61]Liu Jing,Numerical and experimental investigation of fuel spray in supersonic cross flow[D].北京:北京航空航天大学博士论文,2010.
[62]Corin Segal.The Scramjet Engine:Process and Characteristics[M].Cambridge University Press.ISBN 978-7-80243-954-2(2009)
[63]Jinho Lee,Kuo-Cheng Lin,Dean Eklund.Challenges in Fuel Injection for High-Speed Propulsion Systems[J].AIAA JOURNAL,Vol.53,No.6,2015.
© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号 地址：北京市海淀区学院路29号 邮编：100083 电话：办公室：(+86 10)66554848；文献借阅、咨询服务、科技查新：66554700 |