收稿日期:
2023-11-15
修回日期:
2023-11-20
接受日期:
2023-11-24
出版日期:
2024-03-15
发布日期:
2023-12-13
通讯作者:
刘小勇
E-mail:31suoban@sina.com
基金资助:
Xiaoyong LIU(), Mingfu WANG, Jianwen LIU, Xin REN, Xuan ZHANG
Received:
2023-11-15
Revised:
2023-11-20
Accepted:
2023-11-24
Online:
2024-03-15
Published:
2023-12-13
Contact:
Xiaoyong LIU
E-mail:31suoban@sina.com
Supported by:
摘要:
自20世纪50年代以来,航空航天领域把超燃冲压发动机作为高超声速推进系统的一种追求目标,在理论和技术方面矢志不渝地开展了大量研究工作。21世纪初,美国取得了一系列接近实际应用的技术突破,将超燃冲压发动机技术的研究和应用推动至新阶段。简述了超燃冲压发动机工作原理,论述了双模态工作过程、高超声速压缩流动、超声速燃烧、超高温结构与热防护、地面试验与数值模拟等关键技术的难点和新进展,并针对超燃冲压发动机宽速域、可重复和更高马赫数等当前重点技术发展方向,阐述了认识和建议。
中图分类号:
刘小勇, 王明福, 刘建文, 任鑫, 张轩. 超燃冲压发动机研究回顾与展望[J]. 航空学报, 2024, 45(5): 529878-529878.
Xiaoyong LIU, Mingfu WANG, Jianwen LIU, Xin REN, Xuan ZHANG. Review and prospect of research on scramjet[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529878-529878.
1 | PRISELL E. The scramjet: A solution for hypersonic aerodynamic propulsion[C]∥Proceedings of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2005. |
2 | SEEBASS A R. Review and evaluation of the air force hypersonic technology program: AFSB TR-J-97-01-A[R]. Washington, D.C.: National Academy Press, 1998. |
3 | KILLACKEY J J, KATINSZKY E A, VUIGNER A A, et al. Thermal-structural design study of an airframe-integrated scramjet final report: NASA-CR-159039[R]. Washington, D.C.: NASA,1980. |
4 | 刘小勇. 超燃冲压发动机技术[J]. 飞航导弹, 2003(2): 38-42. |
LIU X Y. Scramjet technology[J]. Winged Missiles Journal, 2003(2): 38-42 (in Chinese). | |
5 | 陈扶鼎. 2022年国外高超声速武器发展回顾[J]. 中国航天, 2023(2): 31-37. |
CHEN F D. Review of the development of hypersonic weapons abroad in 2022[J]. Aerospace China, 2023(2): 31-37 (in Chinese). | |
6 | CONNORS J F, MEYERS R C. Design criteria for axisymmetric and two-dimensional supersonic inlets and exits: NACA TN-3589[R]. Washington, D.C.: NACA, 1956. |
7 | MOLDER S, MCGREGOR R J, PAISLEY T W. A comparison of three hypersonic air inlets [R]. Toronto: Ryerson Poly technical Institute, 1991. |
8 | MCCLINTON C R, RAUSCH D R. Hyper-X program status: AIAA-2001-1910[R]. Reston: AIAA, 2001. |
9 | MOSES P L, RAUSCH V L, NGUYEN L T, et al. NASA hypersonic flight demonstrators—Overview, status, and future plans[J]. Acta Astronautica, 2004, 55(3-9): 619-630. |
10 | TREXLER C A. Performance of an inlet for an integrated scramjet concept[J]. Journal of Aircraft, 1974, 11(9): 589-591. |
11 | TREXLER C, SOUDERS S. Design and performance at a local Mach number of 6 of an inlet for an integrated Scramjet concept: NASA TM-7944[R]. Washington, D. C.: NASA, 1975. |
12 | 李怡庆, 周驯黄, 朱呈祥, 等. 曲锥前体/三维内转进气道一体化设计与分析[J].航空动力学报, 2018, 33(1):87-96. |
LI Q Y, ZHOU X H, ZHU C X, et al. Integration design and analysis for curved conical forebody and three-dimensional inward turning inlet[J]. Journal of Aerospace Power, 2018, 33(1): 87-96 (in Chinese). | |
13 | BILLIG F. SCRAM—A supersonic combustion ramjet missile[C]∥Proceedings of the 29th Joint Propulsion Conference and Exhibit. Reston: AIAA, 1993. |
14 | SMART M, WHITE J. Computational investigation of the performance and back-pressure limits of a hypersonic inlet[C]∥Proceedings of the 40th AIAA Aerospace Sciences Meeting & Exhibit. Reston: AIAA, 2002. |
15 | MOLDER S, SZPIRO E J. Busemann inlet for hypersonic speeds[J]. Journal of Spacecraft and Rockets, 1966, 3(8): 1303-1304. |
16 | WALTRUP P J, BILLIG F S. Structure of shock waves in cylindrical ducts[J]. AIAA Journal, 1973, 11(10): 1404-1408. |
17 | BEMENT D, STEVENS J, THOMPSON M. Measured operating characteristics of a rectangular combustor/inlet isolator[C]∥Proceedings of the 26th Joint Propulsion Conference. Reston: AIAA, 1990. |
18 | 王渊, 张堃元, 张林, 等. 非对称超声速来流下矩形转圆隔离段研究[J]. 推进技术, 2014, 35(11): 1448-1454. |
WANG Y, ZHANG K Y, ZHANG L, et al. Investigation on rectangular-to-circular isolator under asymmetric incoming supersonic flow[J]. Journal of Propulsion Technology, 2014, 35(11): 1448-1454 (in Chinese). | |
19 | ZHANG K, MEIER G. Using R.C. method to study optimum compression surface under non-uniform 2-D supersonic flow condition[C]∥Proceedings of the 12th Applied Aerodynamics Conference. Reston: AIAA, 1994. |
20 | ZHANG Y, TAN H J, TIAN F C, et al. Control of incident shock/boundary-layer interaction by a two-dimensional bump[J]. AIAA Journal, 2014, 52(4): 767-776. |
21 | 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. |
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 (in Chinese). | |
22 | YU X F, PAN X, ZHENG J L, et al. Thermodynamic spectrum of direct precooled airbreathing propulsion[J]. Energy, 2017, 135: 777-787. |
23 | SIEBENHAAR A, BOGAR T. The impact of round combustors on TBCC propulsion and hypersonic cruise vehicles[C]∥Proceedings of the 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2006. |
24 | FAULKNER R. The evolution of the HySET hydrocarbon fueled scramjet engine: AIAA-2003-7005[R]. Reston: AIAA, 2003. |
25 | 孙强, 王健, 马会民. X-51A超燃冲压发动机的研制历程[J]. 飞航导弹, 2011(1): 67-71. |
SUN Q, WANG J, MA H M. Development of X-51A scramjet[J]. Aerodynamic Missile Journal, 2011(1): 67-71 (in Chinese). | |
26 | BILLIG F, BAURLE R, TAM C J, et al. Design and analysis of streamline traced hypersonic inlets[C]∥Proceedings of the 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 1999. |
27 | CURRAN E T, MURTHY S N B. High-speed flight propulsion systems[M]. Reston: AIAA, 1991. |
28 | BREIDENTHAL R E. Sonic eddy-A model for compressible turbulence[J]. AIAA Journal, 1992, 30(1): 101-104. |
29 | WEBER R J, MACKAY J S. An analysis of ramjet engines using supersonic combustion: NACA-TN-4386[R]. Washington, D.C.: NACA, 1958. |
30 | 俞刚, 范学军. 超声速燃烧与高超声速推进[J]. 力学进展, 2013, 43(5): 449-470. |
YU G, FAN X J. Supersonic combustion and hypersonic propulsion[J]. Advances in Mechanics, 2013, 43(5): 449-470 (in Chinese). | |
31 | CURRAN E T, MURTHY S N B. Scramjet propulsion[M]. Reston: AIAA, 2000. |
32 | BRINK D F, CHOW W L. Two-dimensional jet mixing with a pressure gradient[J]. Journal of Applied Mechanics, 1975, 42(1): 55-60. |
33 | BROWAND F K. The structure of the turbulent mixing layer[J]. Physica D: Nonlinear Phenomena, 1986, 18(1-3): 135-148. |
34 | CROWE C T, CHUNG J N, TROUTT T R. Particle mixing in free shear flows[J]. Progress in Energy and Combustion Science, 1988, 14(3): 171-194. |
35 | MARCU B, MEIBURG E, RAJU N. The effect of streamwise braid vortices on the particle dispersion in a plane mixing layer. II. Nonlinear particle dynamics[J]. Physics of Fluids, 1996, 8(3): 734-753. |
36 | MARCU B, MEIBURG E. Three-dimensional features of particle dispersion in a nominally plane mixing layer[J]. Physics of Fluids, 1996, 8(9): 2266-2268. |
37 | MARCU B, MEIBURG E. The effect of streamwise braid vortices on the particle dispersion in a plane mixing layer. I. Equilibrium points and their stability[J]. Physics of Fluids, 1996, 8(3): 715-733. |
38 | BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of fuel-air mixtures[J]. Combustion, Explosion and Shock Waves, 2006, 42(4): 463-471. |
39 | ROUTOVSKY V. Autoignition study on kerosene combustion in supersonic flow: F61708-96-WO286[R]. Moscow: Moscow State Aviation Institute, 1997. |
40 | GOKULAKRISHNAN P, GAINES G, KLASSEN M, et al. Autoignition of aviation fuels: experimental and modeling study[C]∥Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2007. |
41 | TAKITA K, MASUYA G, SATO T, et al. Effects of addition of radicals supplied by plasma torch on burning velocity[C]∥Proceedings of the 35th Joint Propulsion Conference and Exhibit. Reston: AIAA, 1999. |
42 | COLKET M B III, SPADACCINI L J. Scramjet fuels autoignition study[J]. Journal of Propulsion and Power, 2001, 17(2): 315-323. |
43 | SEINER J, DASH S, KENZAKOWSKI D. Historical survey on enhanced mixing in scramjet engines[C]∥Proceedings of the 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 1999. |
44 | YAKAR B A. Experimental investigation of mixing and ignition of transverse jets in supersonic crossflows[D]. Stanford: Stanford University, 2000. |
45 | STALLINGS R L, WILCOX E J. Experimental cavity pressure distributions at supersonic speeds: NASA-TP-2683[R]. Washington, D.C.: NASA, 1987. |
46 | ROUDAKOV A S, SEMENOV V L, HICKS J. Recent flight test results of the joint CIAM-NASA Mach 6.5 scramjet flight program: AIAA-1998-1643[R]. Reston: AIAA, 1998. |
47 | VINOGRADOV V, KOBIGSKY S A, PETROV M. Experimental investigation of liquid carbonhydrogen fuel combustion in channel at supersonic velocities: AIAA-1992-3429[R]. Reston: AIAA, 1992. |
48 | KANDA T. Study of the intensive combustion in the scramjet engine[C]∥Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 1998. |
49 | GRUBER M R. An experimental investigation of transverse injection from circular and elliptical nozzles into a supersonic crossflow[D]. Urbana-Champaign: University of Illinois, 1996. |
50 | VANLERBERGHE W M, SANTIAGO J G, DUTTON J C, et al. Mixing of a sonic transverse jet injected into a supersonic flow[J]. AIAA Journal, 2000, 38: 470-479. |
51 | BAURLE R, TAM C J, DASGUPTA S. Analysis of unsteady cavity flows for scramjet applications[C]∥Proceedings of the 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 2000. |
52 | DAVIS D L. Numerical analysis of two and three dimensional recessed flame holders for scramjet applications[D]. Wright-Patterson AFB: Air Force Institute of Technology, 1996. |
53 | FAN T, TIAN M, EDWARDS J, et al. Validation of a hybrid Reynolds-averaged/large-eddy simulation method for simulating cavity flameholder configurations[C]∥ Proceedings of the 15th AIAA Computational Fluid Dynamics Conference. Reston: AIAA, 2001. |
54 | BEN-YAKAR A, HANSON R. Supersonic combustion of cross-flow jets and the influence of cavity flame-holders[C]∥Proceedings of the 37th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1999. |
55 | YU K, WILSON K, SCHADOW K. Effect of flame-holding cavities on supersonic combustion performance[C]∥Proceedings of the 35th Joint Propulsion Conference and Exhibit. Reston: AIAA, 1999. |
56 | MORRISON C Q, CAMPBELL R L, EDELMAN R B, et al. Hydrocarbon fueled dual-mode ramjet/scramjet concept evaluation: ISABE 1997-7053[R]. Indianapolis: ISABE, 1997. |
57 | RASMUSSEN C, DRISCOLL J, DONBAR J, et al. Blowout limits of supersonic cavity-stabilized flames[C]∥Proceedings of the 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 2004. |
58 | YU G. Characterization of kerosene combustion in supersonic flow using effervescent atomization: AIAA-2002-5225[R]. Reston: AIAA, 2002. |
59 | LI M L, ZHOU J, GENG H, et al. Investigations on function of cavity in supersonic combustion using OH PLIF[C]∥Proceedings of the 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 2004. |
60 | MCCLINTON C, ROUDAKOV A, SEMENOV V, et al. Comparative flow path analysis and design assessment of an axisymmetric hydrogen fueled scramjet flight test engine at a Mach number of 6.5[C]∥Proceedings of the Space Plane and Hypersonic Systems and Technology Conference. Reston: AIAA, 1996. |
61 | CHOI Y, YOST M F, LERNER E W, et al. Scramjet performance computed for a JP-7-fueled generic X-51 vehicle[J]. Journal of Propulsion and Power, 2022, 38(3): 348-358. |
62 | FREEBORN A, KING P, GRUBER M. Characterization of pylon effects on a scramjet cavity flameholder flowfield[C]∥Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2008. |
63 | GHODKE C, CHOI J, SRINIVASAN S, et al. Large eddy simulation of supersonic combustion in a cavity-strut flameholder[C]∥Proceedings of the 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2011. |
64 | HEISER W, PRATT D, DALEY D, et al. Hypersonic airbreathing propulsion[M]. Reston: AIAA,1994. |
65 | ANDREADIS D. Scramjets integrate air and space[R]. College Park: American Institute of Physics, 2004. |
66 | 叶中元, 黄伏军, 董建明. 多模态冲压发动机提高性能的技术途径[J]. 推进技术, 2001, 22(6): 441-445, 450. |
YE Z Y, HUANG F J, DONG J M. Development and innovation of multi-mode ramjet technology[J]. Journal of Propulsion Technology, 2001, 22(6): 441-445, 450 (in Chinese). | |
67 | 王兰, 邢建文, 郑忠华, 等. 超燃冲压发动机内流性能的一维评估[J]. 推进技术, 2008, 29(6): 641-645. |
WANG L, XING J W, ZHENG Z H, et al. One-dimensional evaluation of the scramjet flowpath performance[J]. Journal of Propulsion Technology, 2008, 29(6): 641-645 (in Chinese). | |
68 | 任鑫, 罗春钦, 董建明, 等. 超燃冲压发动机性能的准二维计算方法[J]. 推进技术, 2013, 34(4): 457-462. |
REN X, LUO C Q, DONG J M, et al. Quasi-two-dimensional evaluation of the scramjet performance[J]. Journal of Propulsion Technology, 2013, 34(4): 457-462 (in Chinese). | |
69 | 罗世彬, 罗文彩, 王振国. 基于并联协作混合遗传算法的高超声速巡航飞行器一体化优化设计研究[J]. 宇航学报, 2004, 25(1): 28-34. |
LUO S B, LUO W C, WANG Z G. Parallel collaborative hybrid genetic algorithm applied to integrated design optimization of hypersonic cruise vehicle[J]. Journal of Astronautics, 2004, 25(1): 28-34 (in Chinese). | |
70 | 吴先宇, 李小山, 丁猛, 等. 超燃冲压发动机燃烧室构型优化的试验研究[J]. 国防科技大学学报, 2007, 29(5): 1-4, 47. |
WU X Y, LI X S, DING M, et al. Experimental study of the configuration optimization of scramjet combustor[J]. Journal of National University of Defense Technology, 2007, 29(5): 1-4, 47 (in Chinese). | |
71 | 王友利, 才满瑞. 美国X-51A项目总结与前景分析[J]. 飞航导弹, 2014(3): 17-21. |
WANG Y L, CAI M R. Summary and prospect analysis of American X-51A project[J]. Aerodynamic Missile Journal, 2014(3): 17-21 (in Chinese). | |
72 | CURRAN E T, STULL F D. The utilization of supersonic combustion ramjet systems at low Mach numbers: RTD-TDR-63-4097[R]. Wright-Patterson AFB: Aero Propulsion Laboratory, 1964. |
73 | MARSHALL L, BAHM C, CORPENING G, et al. Overview with results and lessons learned of the X-43A Mach 10 flight: AIAA-2005-3336[R]. Reston: AIAA, 2005. |
74 | MAYER D. X-51A waverider achieves breakthrough in final flight[R]. Washington, D.C.: U. S. Department of Defense Information, 2013. |
75 | MA J, LIANG J L. Development trends and directions of liquid ramjet/scramjet technology[J]. Journal of Rocket Propulsion, 2011, 37(4): 12-17 (in Chinese). |
76 | REN J W, TAN Y H. Thermal protection techniques of ramjet combustor[J]. Journal of Rocket Propulsion, 2006, 32(4): 38-42. |
77 | VAN WIE D M, DREWRY D G Jr, KING D E, et al. The hypersonic environment: Required operating conditions and design challenges[J]. Journal of Materials Science, 2004, 39(19): 5915-5924. |
78 | 任富建, 刘红娟, 沈毅. C/C复合材料高温抗氧化性的研究进展[J]. 中国陶瓷工业, 2007, 14(5): 28-31. |
REN F J, LIU H J, SHEN Y. Progress in the study on oxidation resistance of carbon/carbon composites at high temperature[J]. China Ceramic Industry, 2007, 14(5): 28-31 (in Chinese). | |
79 | 葛毅成, 易茂中, 黄伯云. 溶液浸渍和溶胶浸渍法对C/C复合材料抗氧化性能的影响[J]. 粉末冶金材料科学与工程, 2003, 8(2): 156-161. |
GE Y C, YI M Z, HUANG B Y. Effect of anti-oxidation on C/C composites by sol-soaking and solution-soaking[J]. Materials Science and Engineering of Powder Metallargy, 2003, 8(2): 156-161 (in Chinese). | |
80 | 曾燮榕, 李贺军, 张建国, 等. 碳/碳复合材料防护涂层的抗氧化行为研究[J]. 复合材料学报, 2000, 17(2): 42-45. |
ZENG X R, LI H J, ZHANG J G, et al. Effect of microstructure and component on oxidation resistance of MoSi2-SiC multilayer ceramic coating[J]. Acta Materiae Compositae Sinica, 2000, 17(2): 42-45 (in Chinese). | |
81 | 侯党社, 李克智, 李贺军, 等. C/C复合材料SiC-TaSi2/MoSi2抗氧化复合涂层研究[J]. 金属学报, 2008, 44(3): 331-335. |
HOU D S, LI K Z, LI H J, et al. Study of the SiC-TaSi2/MoSi2 multilayer oxidation protective coating for carbon/carbon composite[J]. Acta Metallurgica Sinica, 2008, 44(3): 331-335 (in Chinese). | |
82 | 李贺军. 炭/炭复合材料[J]. 新型炭材料, 2001, 16(2): 79-80. |
LI H J. Carbon/carbon composites[J]. New Carbon Materials, 2001, 16(2): 79-80 (in Chinese). | |
83 | ALFANO D. Spectroscopic properties of carbon fibre reinforced silicon carbide composites for aerospace applications[M]∥GERHARDT R. Properties and Applications of Silicon Carbide. London: IntechOpen, 2011: 231-250. |
84 | HEIDENREICH B. Carbon fiber reinforced SiC materials based on melt infiltration[C]∥6th International Conference on High Temperature Ceramic Matrix Composites, 2007. |
85 | 邹武, 张康助, 张立同. 陶瓷基复合材料在火箭发动机上的应用[J]. 固体火箭技术, 2000, 23(2): 60-64, 68. |
ZOU W, ZHANG K Z, ZHANG L T. Application of ceramic matrix composite to rocket motor[J]. Journal of Solid Rocket Technology, 2000, 23(2): 60-64, 68 (in Chinese). | |
86 | ZHANG X H, HU P, HAN J C. Structure evolution of ZrB2-SiC during the oxidation in air[J]. Journal of Materials Research, 2008, 23(7): 1961-1972. |
87 | 闫联生, 王涛, 邹武, 等. 碳/碳化硅复合材料快速成型工艺研究[J]. 宇航材料工艺, 1999, 29(3): 38-41, 45. |
YAN L S, WANG T, ZOU W, et al. Study on rapid prototyping technology of carbon/silicon carbide composites[J]. Aerospace Materials & Technology, 1999, 29(3): 38-41, 45 (in Chinese). | |
88 | SALAKHUTDINOV G M. Development of methods of cooling liquid propellant rocket engines (ZhRDs), 1903-1970[M]. SKOOG A I. History of Rocketry and Astronautics. San Diego: American Astronautics Society, 1990: 115-122. |
89 | 程泽源, 朱剑琴, 金钊. 吸热型碳氢燃料RP-3替代模型研究[J]. 航空动力学报, 2016, 31(2): 391-398. |
CHENG Z Y, ZHU J Q, JIN Z. Study on surrogate model of endothermic hydrocarbon fuel RP-3[J]. Journal of Aerospace Power, 2016, 31(2): 391-398 (in Chinese). | |
90 | MAURICE L Q, LANDER H, EDWARDS T, et al. Advanced aviation fuels: A look ahead via a historical perspective[J]. Fuel, 2001, 80(5): 747-756. |
91 | STIEGEMEIER B, MEYER M, TAGHAVI R. A thermal stability and heat transfer investigation of five hydrocarbon fuels[C]∥Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2002. |
92 | 王彦红, 李素芬, 东明. 方形再生冷却通道内超临界正癸烷湍流传热数值研究[J]. 推进技术, 2015, 36(11): 1669-1676. |
WANG Y H, LI S F, DONG M. Numerical study on turbulent heat transfer of supercritical n-decane in a square regenerative cooling channel[J]. Journal of Propulsion Technology, 2015, 36(11): 1669-1676 (in Chinese). | |
93 | 姜蕾, 刘朝晖, 毕勤成, 等. 碳氢燃料变压力过程中传热研究[J]. 推进技术, 2014, 35(7): 965-972. |
JIANG L, LIU Z H, BI Q C, et al. Heat transfer of hydrocarbon fuel during transient pressure[J]. Journal of Propulsion Technology, 2014, 35(7): 965-972 (in Chinese). | |
94 | EDWARDS T. Cracking and deposition behavior of supercritical hydrocarbon aviation fuels[J]. Combustion Science and Technology, 2006, 178(1-3): 307-334. |
95 | 张其翼, 魏微, 周灏, 等. 碳氢燃料低压裂解特性[J]. 燃烧科学与技术, 2015, 21(5): 383-386. |
ZHANG Q Y, WEI W, ZHOU H, et al. Pyrolysis characteristics of hydrocarbon fuel under low pressure[J]. Journal of Combustion Science and Technology, 2015, 21(5): 383-386 (in Chinese). | |
96 | STIEGEMEIER B, MEYER M, TAGHAVI R. A thermal stability and heat transfer investigation of five hydrocarbon fuels[C]∥Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2002. |
97 | ZHANG C B, XU G Q, GAO L, et al. Experimental investigation on heat transfer of a specific fuel (RP-3) flows through downward tubes at supercritical pressure[J]. The Journal of Supercritical Fluids, 2012, 72: 90-99. |
98 | 王宁. 超燃冲压发动机再生冷却通道内煤油流动与传热特性研究[D]. 长沙: 国防科学技术大学, 2014. |
WANG N. Study on flow and heat transfer characteristics of kerosene in regenerative cooling channel of scramjet[D].Changsha: National University of Defense Technology, 2014 (in Chinese). | |
99 | RUAN B, MENG H, YANG V. Simplification of pyrolytic reaction mechanism and turbulent heat transfer of n-decane at supercritical pressures[J]. International Journal of Heat and Mass Transfer, 2014, 69: 455-463. |
100 | LIU X Y, YANG Z Q, MIAO R P, et al. Experimental study on flow excursion instability of supercritical hydrocarbon fuel in scramjet regenerative cooling parallel channels[J]. Chinese Journal of Aeronautics, 2023, 36(1): 201-215. |
101 | 郭永胜, 林瑞森. 吸热型碳氢燃料的结焦研究Ⅰ含硫抑制剂[J]. 燃料化学学报, 2005, 33(3): 289-292. |
GUO Y S, LIN R S. Study on coking of endothermic hydrocarbon fuels Ⅰ Sulf-inhibitor[J]. Journal of Fuel Chemistry and Technology, 2005, 33(3): 289-292 (in Chinese). | |
102 | BALSTER L M, CORPORAN E, DEWITT M J, et al. Development of an advanced, thermally stable, coal-based jet fuel[J]. Fuel Processing Technology, 2008, 89(4): 364-378. |
103 | HENEGHAN S P, ZABARNICK S, BALLAL D R, et al. JP-8+100: The development of high-thermal-stability jet fuel[J]. Journal of Energy Resources Technology, 1996, 118(3): 170-179. |
104 | GUO W, ZHANG X W, LIU G Z, et al. Roles of hydrogen donors and organic selenides in inhibiting solid deposits from thermal stressing of n-dodecane and Chinese RP-3 jet fuel[J]. Industrial & Engineering Chemistry Research, 2009, 48(18): 8320-8327. |
105 | MAURICE L, CORPORAN E, MINUS D, et al. Smart fuels-‘Controlled’ chemically reacting[C]∥Proceedings of the 9th International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 1999. |
106 | HUANG B, SHRESTHA U, DAVIS R J, et al. Endothermic pyrolysis of JP-10 with and without zeolite catalyst for hypersonic applications[J]. AIAA Journal, 2018, 56(4): 1616-1626. |
107 | JIANG R P, LIU G Z, ZHANG X W. Thermal cracking of hydrocarbon aviation fuels in regenerative cooling microchannels[J]. Energy & Fuels, 2013, 27(5): 2563-2577. |
108 | KORABELNIKOV A, KURANOV A. Thermochemical conversion of hydrocarbon fuel for the AJAX concept[C]∥Proceedings of the 30th Plasmadynamic and Lasers Conference. Reston: AIAA, 1999. |
109 | JACKSON K, CORPORAN E, BUCKLEY P, et al. Test results of an endothermic fuel reactor: AIAA-1995-6028[R]. Reston: AIAA, 1995. |
110 | LEE P H, LEE S Y, KWON J Y, et al. Thermal cycling behavior and interfacial stability in thick thermal barrier coatings[J]. Surface and Coatings Technology, 2010, 205(5): 1250-1255. |
111 | VASSEN R, STUKE A, STÖVER D. Recent developments in the field of thermal barrier coatings[J]. Journal of Thermal Spray Technology, 2009, 18(2): 181-186. |
112 | MILLER R A. Current status of thermal barrier coatings—An overview[J]. Surface and Coatings Technology, 1987, 30(1): 1-11. |
113 | CAO X Q, VASSEN R, STOEVER D. Ceramic materials for thermal barrier coatings[J]. Journal of the European Ceramic Society, 2004, 24(1): 1-10. |
114 | 郭洪波, 宫声凯, 徐惠彬. 先进航空发动机热障涂层技术研究进展[J]. 中国材料进展, 2009, 28(): 18-26. |
GUO H B, GONG S K, XU H B. Research progress of thermal barrier coating technology for advanced aero-engines[J]. Materials China, 2009, 28(Sup 2): 18-26 (in Chinese). | |
115 | ZHU D M, MILLER R A. Development of advanced low conductivity thermal barrier coatings[J]. International Journal of Applied Ceramic Technology, 2004, 1(1): 86-94. |
116 | 冀晓鹃, 宫声凯, 徐惠彬, 等. 添加稀土元素对热障涂层YSZ陶瓷层晶格畸变的影响[J]. 航空学报, 2007, 28(1): 196-200. |
JI X J, GONG S K, XU H B, et al. Influence of rare earth elements additions in YSZ ceramic coatings of thermal barrier coatings on lattice distortion[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(1): 196-200 (in Chinese). | |
117 | 冀晓鹃. 稀土氧化物掺杂改性热障涂层用YSZ陶瓷材料研究[D]. 北京: 北京航空航天大学, 2007. |
JI X J. Study on YSZ ceramic materials for rare earth oxide doped modified thermal barrier coating[D]. Beijing: Beihang University, 2007 (in Chinese). | |
118 | ZHANG Y L, GUO L, YANG Y P, et al. Influence of Gd2O3 and Yb2O3 co-doping on phase stability, thermo-physical properties and sintering of 8YSZ[J]. Chinese Journal of Aeronautics, 2012, 25(6): 948-953. |
119 | 陈玉峰, 王广海, 郑日恒, 等. 一种超高温隔热材料及其制备方法: CN103626472B[P]. 2015-10-28. |
CHEN Y F, WANG G H, ZHENG R H, et al. Ultra-high-temperature heat-insulating material and preparation method thereof: CN103626472B[P]. 2015-10-28 (in Chinese). | |
120 | 陈玉峰, 张世超, 郑日恒, 等. 带有辐射屏蔽层的纳米氧化硅隔热材料及其制备方法: CN103693938B[P]. 2016-03-23. |
CHEN Y F, ZHANG S C, ZHENG R H, et al. Nano silicon oxide heat-insulating material with radiation shield layer and preparation method thereof: CN103693938B [P]. 2016-03-23 (in Chinese). | |
121 | 韩丁, 郑世刚, 孙现凯, 等. 氧化锆纤维高温隔热材料传热性能研究[J]. 陶瓷, 2022(7): 9-12. |
HAN D, ZHENG S G, SUN X K, et al. Study on heat transfer performance of zirconia ceramic fiber thermal insulation material at high temperature[J]. Ceramics, 2022(7): 9-12 (in Chinese). | |
122 | 陈玉峰, 洪长青, 胡成龙, 等. 空天飞行器用热防护陶瓷材料[J]. 现代技术陶瓷, 2017, 38(5): 311-390. |
CHEN Y F, HONG C Q, HU C L, et al. Ceramic-based thermal protection materials for aerospace vehicles[J]. Advanced Ceramics, 2017, 38(5): 311-390 (in Chinese). | |
123 | 史超. 冲压发动机地面试验技术及试验能力述评[J]. 火箭推进, 2021, 47(1): 1-12. |
SHI C. Review of ramjet ground-test facilities and relevant technology development[J]. Journal of Rocket Propulsion, 2021, 47(1): 1-12 (in Chinese). | |
124 | ADRIAN R J. Particle-imaging techniques for experimental fluid mechanics[J]. Annual Review of Fluid Mechanics, 1991, 23: 261-304. |
125 | 徐惊雷. PIV技术在超及高超声速流场测量中的研究进展[J]. 力学进展, 2012, 42(1): 81-90. |
XU J L. The development of the PIV experimental study of the super/hypersonic flowfield[J]. Advances in Mechanics, 2012, 42(1): 81-90 (in Chinese). | |
126 | HANSON R K. Applications of quantitative laser sensors to kinetics, propulsion and practical energy systems[J]. Proceedings of the Combustion Institute, 2011, 33(1): 1-40. |
127 | 陈帆, 陶波, 黄斌, 等. 基于TDLAS的脉冲爆震火箭发动机尾焰参数测量[J]. 燃烧科学与技术, 2013, 19(6): 501-506. |
CHEN F, TAO B, HUANG B, et al. Measurement of PDRE plume based on TDLAS technology[J]. Journal of Combustion Science and Technology, 2013, 19(6): 501-506 (in Chinese). | |
128 | PENG J B, CAO Z, YU X, et al. Analysis of combustion instability of hydrogen fueled scramjet combustor on high-speed OH-PLIF measurements and dynamic mode decomposition[J]. International Journal of Hydrogen Energy, 2020, 45(23): 13108-13118. |
129 | 吴戈, 李韵, 万明罡, 等. 平面激光诱导荧光技术在超声速燃烧火焰结构可视化中的应用[J]. 实验流体力学, 2020, 34(3): 70-77. |
WU G, LI Y, WAN M G, et al. Visualization of flame structure in supersonic combustion by Planar Laser Induced Fluorescence technique[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(3): 70-77 (in Chinese). | |
130 | ZETTERVALL N, FUREBY C. A computational study of ramjet, scramjet and dual-mode ramjet combustion in combustor with a cavity flameholder[C]∥Proceedings of the 2018 AIAA Aerospace Sciences Meeting. Reston: AIAA, 2018. |
131 | WEPLER U, KOSCHEL W. Numerical investigation of turbulent reacting flows in a scramjet combustor model[C]∥Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2002. |
132 | 杨事民, 张建良. 超燃冲压发动机燃烧室流场数值模拟[J]. 航空发动机, 2009, 35(4): 25-28, 11. |
YANG S M, ZHANG J L. Numerical simulation of flow field of a scramjet combustor[J]. Aeroengine, 2009, 35(4): 25-28, 11 (in Chinese). | |
133 | 牛东圣, 侯凌云. 碳氢燃料超声速燃烧的火焰面模型模拟[J]. 工程热物理学报, 2013, 34(10): 1986-1989. |
NIU D S, HOU L Y. Numerical simulation of hydrocarbon fuel supersonic combustion using flamelet modeling[J]. Journal of Engineering Thermophysics, 2013, 34(10): 1986-1989 (in Chinese). | |
134 | 樊孝峰, 王江峰, 赵法明, 等. 煤油简化化学反应机理在超燃数值模拟中的应用[J]. 空气动力学学报, 2018, 36(6): 974-982. |
FAN X F, WANG J F, ZHAO F M, et al. Applications of reduced reaction mechanism for numerical calculations in supersonic combustion of kerosene fuel[J]. Acta Aerodynamica Sinica, 2018, 36(6): 974-982 (in Chinese). | |
135 | 樊孝峰, 王江峰, 赵法明, 等. 气态煤油超声速燃烧简化化学反应模型[J]. 国防科技大学学报, 2019, 41(1): 48-57. |
FAN X F, WANG J F, ZHAO F M, et al. Reduced kinetic model for supersonic combustion of vaporized kerosene[J]. Journal of National University of Defense Technology, 2019, 41(1): 48-57 (in Chinese). | |
136 | 陈兵, 张岩, 徐旭. 基于火焰面模型的超声速湍流燃烧数值模拟研究[J]. 推进技术, 2013, 34(12): 1650-1658. |
CHEN B, ZHANG Y, XU X. Numerical simulation of supersonic turbulent combustion flows based on flamelet model[J]. Journal of Propulsion Technology, 2013, 34(12): 1650-1658 (in Chinese). | |
137 | 刘建文, 熊生伟, 马雪松. 基于DRG和QSSA方法的煤油详细燃烧机理简化[J]. 推进技术, 2011, 32(4): 525-529, 549. |
LIU J W, XIONG S W, MA X S. Reduction of kerosene detailed combustion reaction mechanism based on DRG and QSSA[J]. Journal of Propulsion Technology, 2011, 32(4): 525-529, 549 (in Chinese). | |
138 | ARIBIKE D S, SUSU A A. Kinetics and mechanism of the thermal cracking of n-heptane[J]. Thermochimica Acta, 1988, 127: 247-258. |
139 | ARIBIKE D S, SUSU A A. Mechanistic modeling of the pyrolysis of n-heptane[J]. Thermochimica Acta, 1988, 127: 259-273. |
140 | HERBINET O, MARQUAIRE P M, BATTIN-LECLERC F, et al. Thermal decomposition of n-dodecane: Experiments and kinetic modeling[J]. Journal of Analytical and Applied Pyrolysis, 2007, 78(2): 419-429. |
141 | ZHONG F Q, FAN X J, YU G, et al. Thermal cracking of aviation kerosene for scramjet applications[J]. Science in China Series E: Technological Sciences, 2009, 52(9): 2644-2652. |
142 | MCCLINTON C R. Hypersonic technology past, present and future[R]. 2002. |
143 | CULBERTSON A S, BHAT B. The National Aerospace Initiative (NAI): Technologies for responsive space access[R]. Washington, D.C.: NASA, 2003. |
144 | SIEBENHAAR A, BOGAR T. Integration and vehicle performance assessment of the aerojet “TriJet” combined-cycle engine[C]∥Proceedings of the 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2009. |
145 | ROBERTS K, WILSON D. Analysis and design of a hypersonic scramjet engine with a transition Mach number of 4.00[C]∥Proceedings of the 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2009. |
146 | 吴云, 李应红. 等离子体流动控制与点火助燃研究进展[J]. 高电压技术, 2014, 40(7): 2024-2038. |
WU Y, LI Y H. Progress in research of plasma-assisted flow control, ignition and combustion[J]. High Voltage Engineering, 2014, 40(7): 2024-2038 (in Chinese). | |
147 | 许国梁, 陈帅, 吴春田, 等. 乙醇辅助碳氢燃料催化吸热反应[J]. 含能材料, 2020, 28(5): 416-423. |
XU G L, CHEN S, WU C T, et al. Ethanol-assisted catalytic endothermic reaction of hydrocarbon fuel[J]. Chinese Journal of Energetic Materials, 2020, 28(5): 416-423 (in Chinese). | |
148 | QIN J, ZHOU W X, BAO W, et al. Thermodynamic analysis and parametric study of a closed Brayton cycle thermal management system for scramjet[J]. International Journal of Hydrogen Energy, 2010, 35(1): 356-364. |
149 | QIN J, BAO W, ZHOU W X, et al. Thermal management system performance analysis of hypersonic vehicle based on closed Brayton cycle[C]∥Proceedings of the 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston: AIAA, 2008. |
150 | CHENG K L, QIN J, SUN H C, et al. Performance assessment of a closed-recuperative-Brayton-cycle based integrated system for power generation and engine cooling of hypersonic vehicle[J]. Aerospace Science and Technology, 2019, 87: 278-288. |
151 | KATOH Y, SNEAD L L, HENAGER C H, et al. Current status and recent research achievements in SiC/SiC composites[J]. Journal of Nuclear Materials, 2014, 455(1-3): 387-397. |
152 | LACOMBE A, SPRIET P, HABAROU G, et al. Ceramic matrix composites to make breakthroughs in aircraft engine performance[C]∥Proceedings of the 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston: AIAA, 2009. |
153 | 王鸣, 董志国, 张晓越, 等. 连续纤维增强碳化硅陶瓷基复合材料在航空发动机上的应用[J]. 航空制造技术, 2014(6): 10-13. |
WANG M, DONG Z G, ZHANG X Y, et al. Application of continuous fiber reinforced ceramic matrix composites in aeroengine[J]. Aeronautical Manufacturing Technology, 2014(6): 10-13 (in Chinese). | |
154 | 岳连捷, 张旭, 张启帆, 等. 高马赫数超燃冲压发动机技术研究进展[J]. 力学学报, 2022, 54(2): 263-288. |
YUE L J, ZHANG X, ZHANG Q F, et al. Research progress on high-mach-number scramjet engine technologies[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(2): 263-288 (in Chinese). | |
155 | URZAY J. Supersonic combustion in air-breathing propulsion systems for hypersonic flight[J]. Annual Review of Fluid Mechanics, 2018, 50: 593-627. |
156 | WALTRUP P J. Upper bounds on the flight speed of hydrocarbon-fueled scramjet-powered vehicles[J]. Journal of Propulsion and Power, 2001, 17(6): 1199-1204. |
157 | LANDER H, NIXON A C. Endothermic fuels for hypersonic vehicles[J]. Journal of Aircraft, 1971, 8(4): 200-207. |
158 | WANG Y Y, CHENG K L, TANG J F, et al. Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement[J]. Aerospace Science and Technology, 2020, 98: 105594. |
159 | LANDSBERG W O, WHEATLEY V, SMART M K, et al. Performance of high Mach number scramjets - Tunnel vs flight[J]. Acta Astronautica, 2018, 146: 103-110. |
160 | PAQUETTE E. Cooled CMC structures for scramjet engine flowpath components[C]∥Proceedings of the AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Reston: AIAA, 2005. |
161 | BOUQUET C, FISCHER R, LUC-BOUHALI A, et al. Fully ceramic composite heat exchanger qualification for advanced combustion chambers[C]∥Proceedings of the AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Reston: AIAA, 2005. |
[1] | 乔竑玮, 梁剑寒, 张林, 孙明波, 陈玉俏. 超声速燃烧中的概率密度函数方法研究进展[J]. 航空学报, 2024, 45(8): 28802-028802. |
[2] | 郑建成, 曲智国, 谭贤四, 李志淮, 朱刚, 李陆军, 刘伟. 基于责任区划分的雷达网探测高超声速目标资源管理[J]. 航空学报, 2024, 45(8): 329022-329022. |
[3] | 戴今钊, 陈海昕. 流场波系引导的三维消波翼优化设计方法[J]. 航空学报, 2024, 45(6): 628942-628942. |
[4] | 杨博, 于贺, 樊子辰. 微观能量分析气动光学效应时变误差的方法[J]. 航空学报, 2024, 45(4): 128703-128703. |
[5] | 纪鉴恒, 蔡尊, 王泰宇, 孙明波, 王振国. 宽速域超燃冲压发动机流动燃烧过程研究进展[J]. 航空学报, 2024, 45(3): 28696-028696. |
[6] | 赖江, 范召林, 王乾, 董思卫, 童福林, 袁先旭. 高超声速有攻角锥裙直接数值模拟[J]. 航空学报, 2024, 45(2): 128610-128610. |
[7] | 李学良, 李创创, 苏伟, 吴杰. 分布式粗糙元对高超声速边界层不稳定性的影响试验[J]. 航空学报, 2024, 45(2): 128627-128627. |
[8] | 熊有德, 李创创, 张振辉, 吴杰. 高超声速风洞自由来流扰动热线测量技术[J]. 航空学报, 2024, 45(10): 129042-129042. |
[9] | 倪炜霖, 王永海, 徐聪, 赤丰华, 梁海朝. 基于强化学习的高超飞行器协同博弈制导方法[J]. 航空学报, 2023, 44(S2): 729400-729400. |
[10] | 于哲峰, 梁世昌, 石卫波, 田得阳, 石安华, 廖东骏, 杨鹰. 类HTV⁃2飞行器光电特性的分析评估技术[J]. 航空学报, 2023, 44(S2): 729465-729465. |
[11] | 马平, 张宁, 石安华, 于哲峰, 梁世昌, 黄洁. 典型微波波段信号在模拟等离子体中的传输特性[J]. 航空学报, 2023, 44(S2): 729476-729476. |
[12] | 陈浩宇, 王彬文, 宋巧治, 李晓东. 热颤振地面模拟试验技术[J]. 航空学报, 2023, 44(8): 227295-227295. |
[13] | 常思源, 肖尧, 李广利, 田中伟, 张凯凯, 崔凯. 翼反角对高压捕获翼构型高超气动特性的影响[J]. 航空学报, 2023, 44(8): 127349-127349. |
[14] | 刘宏康, 陈坚强, 向星皓, 赵雅甜. 改进k-ω-γ转捩模式对不同雷诺数下HIAD的转捩预测[J]. 航空学报, 2023, 44(6): 126868-126868. |
[15] | 杨国涛, 岳振江, 刘莉. 基于自适应采样的高超声速飞行器气动热全局快速预示[J]. 航空学报, 2023, 44(6): 127391-127391. |
阅读次数 | ||||||
全文 |
|
|||||
摘要 |
|
|||||
版权所有 © 航空学报编辑部
版权所有 © 2011航空学报杂志社
主管单位:中国科学技术协会 主办单位:中国航空学会 北京航空航天大学