Citation: | Ding Feng, Liu Jun, Shen Chibing, et al. An overview of waverider design concept in airframe-inlet integration methodology for air-breathing hypersonic vehicles[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(6): 16-26. doi: 10.11729/syltlx20180080 |
[1] |
O'Neill M K L. Optimized scramjet engine integration on a waverider airframe[D]. College Park, MD: University of Maryland College Park, 1992.
|
[2] |
O'Neill M K L, Lewis M J. Optimized scramjet integration on a waverider[J]. Journal of Aircraft, 1992, 29(6):1114-1121. doi: 10.2514/3.56866
|
[3] |
Heiser W H, Pratt D T. Hypersonic airbreathing propulsion[M]. USA:AIAA Inc, 1994.
|
[4] |
Haney J W, Beaulieu W D. Waverider inlet integration issues[R]. AIAA-1994-383, 1994.
|
[5] |
尤延铖, 梁德旺, 郭荣伟, 等.高超声速三维内收缩式进气道/乘波前体一体化设计研究评述[J].力学进展, 2009, 39(5):513-525. doi: 10.3321/j.issn:1000-0992.2009.05.001
You Y C, Liang D W, Guo R W, et al. Overview of the integration of three-dimensional inward turning hypersonic inlet and waverider forebody[J]. Advances in Mechanics, 2009, 39(5):513-525. doi: 10.3321/j.issn:1000-0992.2009.05.001
|
[6] |
Nonweiler T R F. Aerodynamic problems of manned space vehicles[J]. Aeronautical Journal, 1959, 63(585):521-528. http://journals.cambridge.org/abstract_S0368393100071662
|
[7] |
赵桂林, 胡亮, 闻洁, 等.乘波构型和乘波飞行器研究综述[J].力学进展, 2003, 33(3):357-374. doi: 10.3321/j.issn:1000-0992.2003.03.007
Zhao G L, Hu L, Wen J, et al. An overview of the research on waveriders and waverider-derived hypersonic vehicles[J]. Advances in Mechanics, 2003, 33(3):357-374. doi: 10.3321/j.issn:1000-0992.2003.03.007
|
[8] |
Liu J, Ding F, Huang W, et al. Novel approach for designing a hypersonic gliding-cruising dual waverider vehicle[J]. Acta Astronautica, 2014, 102:81-88. doi: 10.1016/j.actaastro.2014.04.024
|
[9] |
Ding F, Liu J, Shen C B, et al. Novel approach for design of a waverider vehicle generated from axisymmetric supersonic flows past a pointed von Karman ogive[J]. Aerospace Science and Technology, 2015, 42:297-308. doi: 10.1016/j.ast.2015.01.025
|
[10] |
Ding F, Shen C B, Liu J, et al. Influence of surface pressure distribution of basic flow field on shape and performance of waverider[J]. Acta Astronautica, 2015, 108:62-78. doi: 10.1016/j.actaastro.2014.11.038
|
[11] |
Ding F, Shen C B, Liu J, et al. Comparison between novel waverider generated from flow past a pointed von Karman ogive and conventional cone-derived waverider[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2015, 229(14):2620-2633. doi: 10.1177/0954410015581404
|
[12] |
Lewis M J. Application of waverider-based configurations to hypersonic vehicle design[R]. AIAA-1991-3304, 1991.
|
[13] |
Lunan D A. Waverider, a revised chronology[R]. AIAA-2015-3529, 2015.
|
[14] |
Stevens D R. Practical considerations in waverider applications[R]. AIAA-1992-4247, 1992.
|
[15] |
Starkey R P, Lewis M J. Critical design issues for airbreathing hypersonic waverider missiles[J]. Journal of Spacecraft and Rockets, 2001, 38(4):510-519. doi: 10.2514/2.3734
|
[16] |
吴颖川, 贺元元, 余安远, 等.展向截断曲面乘波压缩进气道气动布局[J].航空动力学报, 2013, 28(7):1570-1575. http://d.old.wanfangdata.com.cn/Periodical/hkdlxb201307017
Wu Y C, He Y Y, Yu A Y, et al. Aerodynamic layout of spanwise truncated curved waverider compression inlet[J]. Journal of Aerospace Power, 2013, 28(7):1570-1575. http://d.old.wanfangdata.com.cn/Periodical/hkdlxb201307017
|
[17] |
吴颖川, 姚磊, 杨大伟, 等.曲面乘波进气道非设计状态性能研究[J].实验流体力学, 2015, 29(4):26-31. http://www.syltlx.com/CN/abstract/abstract10855.shtml
Wu Y C, Yao L, Yang D W, et al. Off-design performance of osculating curved cone inlet[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(4):26-31. http://www.syltlx.com/CN/abstract/abstract10855.shtml
|
[18] |
Starkey R P, Lewis M J. Simple analytical model for parametric studies of hypersonic waveriders[J]. Journal of Spacecraft and Rockets, 1999, 36(4):516-523. doi: 10.2514/3.27194
|
[19] |
Starkey R P, Lewis M J. Aerodynamics of a box constrained waverider missile using multiple scramjets[R]. AIAA-1999-2378, 1999.
|
[20] |
Starkey R P, Rankins F, Pines D. Coupled waverider/trajectory optimization for hypersonic cruise[R]. AIAA-2005-0530, 2005.
|
[21] |
李怡庆, 韩伟强, 尤延铖, 等.压力分布可控的高超声速进气道/前体一体化乘波设计[J].航空学报, 2016, 37(9):2711-2720. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hkxb201609009
Li Y Q, Han W Q, You Y C, et al. Integration waverider design of hypersonic inlet and forebody with preassigned pressure distribution[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(9):2711-2720. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hkxb201609009
|
[22] |
Javaid K H, Serghides V C. Airframe-propulsion integration methodology for waverider-derived hypersonic cruise aircraft design concepts[J]. Journal of Spacecraft and Rockets, 2005, 42(4):663-671. doi: 10.2514/1.8782
|
[23] |
Javaid K H, Serghides V C. Thrust-matching requirements for the conceptual design of hypersonic waverider vehicles[J]. Journal of Aircraft, 2005, 42(4):1055-1064. doi: 10.2514/1.8729
|
[24] |
Jones J G, Moore K C, Pike J, et al. A method for designing lifting configurations for high supersonic speeds, using axisymmetric flow fields[J]. Ingenieur-Archiv, 1968, 37(1):56-72. doi: 10.1007/BF00532683
|
[25] |
Lobbia M, Suzuki K. Numerical investigation of waverider-derived hypersonic transport configuratioins[R]. AIAA-2003-3804, 2003.
|
[26] |
He X Z, Le J L, Wu Y C. Design of a curved cone derived waverider forebody[R]. AIAA-2009-7423, 2009.
|
[27] |
贺旭照, 倪鸿礼.密切曲面锥乘波体——设计方法与性能分析[J].力学学报, 2011, 43(6):1077-1082. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=CAS201303040000651623
He X Z, Ni H L. Osculating curved cone (OCC) waverider:design methods and performance analysis[J]. Chinese Journal of Theoretical and Applied Mechanics, 2011, 43(6):1077-1082. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=CAS201303040000651623
|
[28] |
贺旭照, 周正, 毛鹏飞, 等.密切曲面内锥乘波前体进气道设计和试验研究[J].实验流体力学, 2014, 28(3):39-44. http://www.syltlx.com/CN/abstract/abstract10732.shtml
He X Z, Zhou Z, Mao P F, et al. Design and experimental study of osculating inward turning cone waverider/inlet (OICWI)[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(3):39-44. http://www.syltlx.com/CN/abstract/abstract10732.shtml
|
[29] |
He X Z, Le J L, Zhou Z, et al. Osculating inward turning cone waverider/inlet (OICWI) design methods and experimental study[R]. AIAA-2012-5810, 2012.
|
[30] |
He X Z, Le J L, Zhou Z, et al. Progress in waverider inlet integration study[R]. AIAA-2015-3685, 2015.
|
[31] |
He X Z, Zhou Z, Qin S, et al. Design and experimental study of a practical osculating inward cone waverider inlet[J]. Chinese Journal of Aeronautics, 2016, 29(6):1582-1590. doi: 10.1016/j.cja.2016.09.007
|
[32] |
周正, 贺旭照, 卫锋, 等.密切曲内锥乘波前体进气道低马赫数性能试验研究[J].推进技术, 2016, 37(8):1455-1460. http://d.old.wanfangdata.com.cn/Periodical/tjjs201608007
Zhou Z, He X Z, Wei F, et al. Experimental studies of osculating inward turning cone waverider forebody inlet (OICWI) at low Mach number conditions[J]. Journal of Propulsion Technology, 2016, 37(8):1455-1460. http://d.old.wanfangdata.com.cn/Periodical/tjjs201608007
|
[33] |
贺旭照, 秦思, 周正, 等.一种乘波前体进气道的一体化设计及性能分析[J].航空动力学报, 2013, 28(6):1270-1276. http://d.old.wanfangdata.com.cn/Periodical/hkdlxb201306011
He X Z, Qin S, Zhou Z, et al. Integrated design and perfor-mance analysis of waverider forebody and inlet[J]. Journal of Aerospace Power, 2013, 28(6):1270-1276. http://d.old.wanfangdata.com.cn/Periodical/hkdlxb201306011
|
[34] |
Lewis M J, Takashima N. Engine/airframe integration for waverider cruise vehicles[R]. AIAA-1993-0507, 1993.
|
[35] |
Takashima N, Lewis M J. Waverider configurations based on non-axisymmetric flow fields for engine-airframe integration[R]. AIAA-1994-0380, 1994.
|
[36] |
Takashima N, Lewis M J. Wedge-cone waverider configuration for engine-airframe integration[J]. Journal of Aircraft, 1995, 32(5):1142-1144. doi: 10.2514/3.46848
|
[37] |
明承东.乘波前体/进气道气动布局设计方法研究[D].南京: 南京航空航天大学, 2013. https://max.book118.com/html/2015/0901/24471073.shtm
Ming C D. Aerodyanmic layout design method of the waverider forebody/inlet configuration[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2013. https://max.book118.com/html/2015/0901/24471073.shtm
|
[38] |
Sobieczky H, Dougherty F C, Jones K. Hypersonic waverider design from given shock waves[C]//Proc of the 1st International Hypersonic Waverider Symposium. 1990.
|
[39] |
Takashima N, Lewis M J. Engine-airframe integration on osculating cone waverider-based vehicle designs[R]. AIAA-1996-2551, 1996.
|
[40] |
O'Brien T F. RBCC engine-airframe integration on an osculating cone waverider vehicle[D]. College Park, MD: University of Maryland College Park, 2001.
|
[41] |
O'Brien T F, Lewis M J. RBCC engine-airframe integration on an osculating cone waverider vehicle[R]. AIAA-2000-3823, 2000.
|
[42] |
O'Brien T F, Lewis M J. Rocket-based combined-cycle engine integration on an osculating cone waverider vehicle[J]. Journal of Aircraft, 2001, 38(6):1117-1123. doi: 10.2514/2.2880
|
[43] |
吕侦军, 王江峰.多级压缩锥导/吻切锥乘波体设计与对比分析[J].北京航空航天大学学报, 2015, 41(11):2103-2109. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=bjhkhtdxxb201511017
Lyu Z J, Wang J F. Design and comparative analysis of multistage compression cone-derived waverider and osculating cone waverider[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11):2103-2109. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=bjhkhtdxxb201511017
|
[44] |
吕侦军, 王江峰, 伍贻兆, 等.多级压缩锥导乘波体设计与分析[J].宇航学报, 2015, 36(5):518-523. doi: 10.3873/j.issn.1000-1328.2015.05.005
Lyu Z J, Wang J F, Wu Y Z, et al. Design and analysis of multistage compression cone-derived waverider configuration[J]. Journal of Astronautics, 2015, 36(5):518-523. doi: 10.3873/j.issn.1000-1328.2015.05.005
|
[45] |
吕侦军, 王旭东, 季卫栋, 等.三级压缩锥导乘波体设计技术与实验分析[J].实验流体力学, 2015, 29(5):38-44. http://www.syltlx.com/CN/abstract/abstract10872.shtml
Lyu Z J, Wang X D, Ji W D, et al. Design and experimental analysis of three-stage compression cone-derived waverider[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(5):38-44. http://www.syltlx.com/CN/abstract/abstract10872.shtml
|
[46] |
Wang X D, Wang J F, Lyu Z J. A new integration method based on the coupling of mutistage osculating cones waverider and Busemann inlet for hypersonic airbreathing vehicles[J]. Acta Astronautica, 2016, 126:424-438. doi: 10.1016/j.actaastro.2016.06.022
|
[47] |
Sobieczky H, Zores B, Wang Z, et al. High speed flow design using osculating axisymmetric flows[C]//Proc of the 3rd Pacific International Conference on Aerospace Science and Technology. 1997.
|
[48] |
Sobieczky H, Zores B, Wang Z, et al. High speed flow design using osculating axisymmetric flows[J]. Chinese Journal of Aeronautics, 1999, 12(1):1-8. http://d.old.wanfangdata.com.cn/Periodical/hkxb-e199901001
|
[49] |
Rodi P E. The osculating flowfield method of waverider geometry generation[R]. AIAA-2005-511, 2005.
|
[50] |
Rodi P E. Engineering-based performance comparisons between osculating cone and osculating flowfield waveriders[R]. AIAA-2007-4344, 2007.
|
[51] |
Rodi P E. Geometrical relationships for osculating cones and osculating flowfield waveriders[R]. AIAA-2011-1188, 2011.
|
[52] |
Rodi P E. Preliminary ramjet/scramjet integration with vehicles using osculating flowfields waverider forebodies[R]. AIAA-2012-3223, 2012.
|
[53] |
You Y C, Zhu C X, Guo J L. Dual waverider concept for the integration of hypersonic inward-turning inlet and airframe forebody[R]. AIAA-2009-7421, 2009.
|
[54] |
Li Y Q, An P, Pan C J, et al. Integration methodology for waverider-derived hypersonic inlet and vehicle forebody[R]. AIAA-2014-3229, 2014.
|
[55] |
南向军, 张堃元, 金志光.乘波前体两侧高超声速内收缩进气道一体化设计[J].航空学报, 2012, 33(8):1417-1426. http://d.old.wanfangdata.com.cn/Periodical/hkxb201208008
Nan X J, Zhang K Y, Jin Z G. Integrated design of waverider forebody and lateral hypersonic inward turning inlets[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(8):1417-1426. http://d.old.wanfangdata.com.cn/Periodical/hkxb201208008
|
[56] |
Walker S H, Rodgers F. Falcon hypersonic technology overview[R]. AIAA-2005-3253, 2005.
|
[57] |
Elvin J D. Integrated inward turning inlets and nozzles for hypersonic air vehicle: USA, 07866599. 2011-01-11.
|
[58] |
崔凯, 胡守超, 李广利, 等.双旁侧进气高超声速飞机概念设计与评估[J].中国科学:技术科学, 2013, 43(10):1085-1093. http://cpfd.cnki.com.cn/Article/CPFDTOTAL-AGLU201211007271.htm
Cui K, Hu S C, Li G L, et al. Conceptural design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets[J]. Science China:Technological Sciences, 2013, 43(10):1085-1093. http://cpfd.cnki.com.cn/Article/CPFDTOTAL-AGLU201211007271.htm
|
[59] |
Cui K, Hu S C, Li G L, et al. Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets[J]. Science China:Technological Sciences, 2013, 56(8):1980-1988. doi: 10.1007/s11431-013-5288-0
|
[60] |
O'Neill M K L, Lewis M J. Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles[J]. Journal of Aircraft, 1993, 30(6):943-952. doi: 10.2514/3.46438
|
[61] |
Tarpley C. The optimization of engine-integrated hypersonic waveriders with steady state flight and static margin constraints[D]. College Park, MD: University of Maryland College Park, 1995.
|
[62] |
Tarpley C, Lewis M J. Optimization of an engine-integrated waverider with steady state flight constraints[R]. AIAA-1995-0848, 1995.
|
[63] |
Smith T R, Bowcutt K G. Integrated hypersonic inlet design: USA, 08256706.2012-09-04.
|
[64] |
Ding F, Liu J, Shen C B, et al. Novel inlet-airframe integration methodology for hypersonic waverider vehicles[J]. Acta Astronautica, 2015, 111:178-197. doi: 10.1016/j.actaastro.2015.02.016
|
[65] |
Tian C, Li N, Gong G H, et al. A parameterized geometry design method for inward turning inlet compatible waverider[J]. Chinese Journal of Aeronautics, 2013, 26(5):1135-1146. doi: 10.1016/j.cja.2013.07.003
|
[66] |
Walker S, Tang M, Morris S, et al. Falcon HTV-3X-A reusable hypersonic test bed[R]. AIAA-2008-2544, 2008.
|