EDWARDS T. Aviation fuel development - past highlights and future prospects[C]// AIAA International Air and Space Symposium and Exposition: The Next 100 Years, Dayton, Ohio. AIAA, 2003: AIAA 2003-2611. doi: 10.2514/6.2003-2611

WANG Z G, WANG Y, ZHANG J Q, et al. Overview of the key technologies of combined cycle engine precooling systems and the advanced applications of micro-channel heat transfer[J]. Aerospace Science and Technology, 2014, 39: 31−39. doi: 10.1016/j.ast.2014.08.008

ZHU Y H, PENG W, XU R N, et al. Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles[J]. Chinese Journal of Aeronautics, 2018, 31(10): 1929−1953. doi: 10.1016/j.cja.2018.06.011

FENG Z G, GUAN C Q, ZHANG H W. An introduction to hypersonic aircraft[M]. Beijing: Beijing Insititute of Technology Press, 2016 (in Chinese).

FAN X J, YU G, LI J G, et al. Performance optimization for supersonic combustion of supercritical and cracked kerosene[J]. Acta Aerodynamica Sinica, 2009, 27(z1): 77−83 (in Chinese). doi: 10.3969/j.issn.0258-1825.2009.z1.014

ZHANG M Z, WANG L, ZHANG Z T, et al. Flame characteristic test study of CoaxialSwirl injector[J]. Journal of Combustion Science and Technology, 2008, 14(1): 1−5 (in Chinese). doi: 10.3321/j.issn:1006-8740.2008.01.001

WANG F, LI L F, ZHANG G T. Influence of geometrical structure of coaxial injector on high-frequency combustion instability for staged combustion LOX/kerosene rocket engine[J]. Journal of Experimental Mechanics, 2012, 27(2): 178−182 (in Chinese).

MISER C, KING P, SCHAUER F. PDE flash vaporization system for hydrocarbon fuel using thrust tube waste heat[C]// 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Tucson, Arizona. AIAA, 2005: AIAA 2005-3511. doi: 10.2514/6.2005-3511

FAN W, FAN Z C, JIN (L /Y), et al. Supercritical jet combustion of aviation kerosene[M]. Beijing: Science Press, 2023 (in Chinese).

ZHOU H P, WEN J, DENG H W, et al. Experiment of multi-component hydrocarbon fuels RP-3 thermal conductivity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(10): 1387−1391 (in Chinese).

EDWARDS T, MAURICE L Q. Surrogate mixtures to represent complex aviation and rocket fuels[J]. Journal of Propulsion and Power, 2001, 17(2): 461−466. doi: 10.2514/2.5765

HUBER M L, LEMMON E W, BRUNO T J. Surrogate mixture models for the thermophysical properties of aviation fuel jet-A[J]. Energy Fuels, 2010, 24(6): 3565−3571. doi: 10.1021/ef100208c

NOMURA H, UJIIE Y, RATH H J, et al. Experimental study on high-pressure droplet evaporation using microgravity conditions[J]. Symposium (International) on Combustion, 1996, 26(1): 1267−1273. doi: 10.1016/s0082-0784(96)80344-4

WANG X J, WANG Y X, YANG V. Geometric effects on liquid oxygen/kerosene bi-swirl injector flow dynamics at supercritical conditions[J]. AIAA Journal, 2017, 55(10): 3467−3475. doi: 10.2514/1.j055952

SUN M B, ZHONG Z, LIANG J H, et al. Experimental investigation on combustion performance of cavity-strut injection of supercritical kerosene in supersonic model combustor[J]. Acta Astronautica, 2016, 127: 112−119. doi: 10.1016/j.actaastro.2016.05.035

ZHANG D R, SHAN F L, HOU L Y. Numerical investigations of supersonic combustion characteristics of thermally cracked fuels at typical pyrolysis temperatures[J]. Aerospace Science and Technology, 2024, 144: 108770. doi: 10.1016/j.ast.2023.108770

JI J H, CAI Z, WANG T Y, et al. Flow and combustion process for wide speed range scramjet: Review[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 028696 (in Chinese). doi: 10.7527/S1000-6893.2023.28696

EDWARDS T. USAF supercritical hydrocarbon fuels interests[C]// 31st Aerospace Sciences Meeting, Reno, NV, USA. AIAA, 1993: AIAA 1993-807. doi: 10.2514/6.1993-807

ZHOU N, KRISHNAN A. Supercritical heat transfer in aircraft fuel systems[C]// 31st Joint Propulsion Conference and Exhibit, San Diego, CA, USA. AIAA, 1995: AIAA 1995-3032. doi: 10.2514/6.1995-3032

FABUSS B M, SMITH J O, LAIT R I, et al. Rapid thermal cracking of n-hexadecane at elevated pressures[J]. Industrial Engineering Chemistry Process Design and Development, 1962, 1(4): 293−299. doi: 10.1021/i260004a011

EDWARDS T. Cracking and deposition behavior of supercritical hydrocarbon aviation fuels[J]. Combustion Science and Technology, 2006, 178(1-3): 307−334. doi: 10.1080/00102200500294346

DENG H W, ZHANG C B, XU G Q, et al. Density measurements of endothermic hydrocarbon fuel at sub- and supercritical conditions[J]. Journal of Chemical Engineering Data, 2011, 56(6): 2980−2986. doi: 10.1021/je200258g

DENG H W, ZHANG C B, XU G Q, et al. Visualization experiments of a specific fuel flow through quartz-glass tubes under both sub- and supercritical conditions[J]. Chinese Journal of Aeronautics, 2012, 25(3): 372−380. doi: 10.1016/s1000-9361(11)60398-1

SUN Q M. Measurement and estimation of critical properties of new aviation fuel[D]. Tianjin: Tianjin University, 2006 (in Chinese).

YU D W, MA W G. Experimental measurement of the thermophysical properties of sub/supercritical aviation kerosene[J]. Journal of Engineering Thermophysics, 2023, 44(9): 2532−2540 (in Chinese).

ZHONG F Q, FAN X J, YU G, et al. Heat transfer of aviation kerosene at supercritical conditions[J]. Journal of Thermophysics and Heat Transfer, 2009, 23(3): 543−550. doi: 10.2514/1.41619

JIN L, FAN W, ZHOU Z, et al. Density measurement and calculation of RP-3 aviation kerosene at sub-and supercritical condition[J]. Journal of Propulsion Technology, 2015, 36(7): 1103−1109 (in Chinese).

ZHANG C B, DENG H W, XU G Q, et al. Enthalpy measurement and heat transfer investigation of RP-3 kerosene at supercritical pressure[J]. Journal of Aerospace Power, 2010, 25(2): 331−335(in Chinese). doi: 10.13224/j.cnki.jasp.2010.02.021

LI Z Z, ZHU H R. Heat transfer characteristics of kerosene in micro-channel under supercritical pressure[J]. Journal of Propulsion Technology, 2011, 32(2): 261−265 (in Chinese). doi: 10.13675/j.cnki.tjjs.2011.02.020

YU G, FAN X J. Supersonic combustion and hypersonic propulsion[J]. Advances in Mechanics, 2013, 43(5): 449−471 (in Chinese). doi: 10.6052/1000-0992-13-037

ZHAO G Z, SONG W Y, ZHANG R L. Numerical method development for conjugated heat transfer of hydrocarbon fuel with thermal cracking at supercritical conditions[J]. Journal of Propulsion Technology, 2014, 35(12): 1639−1644 (in Chinese). doi: 10.13675/j.cnki.tjjs.2014.12.008

SHIRALKAR B S, GRIFFITH P. Deterioration in heat transfer to fluids at supercritical pressure and high heat fluxes[J]. Journal of Heat Transfer, 1969, 91(1): 27−36. doi: 10.1115/1.3580115

HUANG D, LI W. Heat transfer deterioration of aviation kerosene flowing in mini tubes at supercritical pressures[J]. International Journal of Heat and Mass Transfer, 2017, 111: 266−278. doi: 10.1016/j.ijheatmasstransfer.2017.03.117

ZHAO G Z, XIAO B G, LI X F, et al. The influences of flow conditions on heat transfer of supercritical cracked-kerosene[J]. International Journal of Thermal Sciences, 2023, 192: 108437. doi: 10.1016/j.ijthermalsci.2023.108437

YANG Z Q, BI Q C, LIU Z H, et al. Heat transfer to supercritical pressure hydrocarbons flowing in a horizontal short tube[J]. Experimental Thermal and Fluid Science, 2015, 61: 144−152. doi: 10.1016/j.expthermflusci.2014.10.024

LIU S Y, FENG Y, CHU Y C, et al. Numerical study of catalytic steam reforming of aviation kerosene at supercritical pressures[J]. Fuel, 2018, 212: 375−386. doi: 10.1016/j.fuel.2017.10.071

FU Y C, HUANG H R, WEN J, et al. Experimental investigation on convective heat transfer of supercritical RP-3 in vertical miniature tubes with various diameters[J]. International Journal of Heat and Mass Transfer, 2017, 112: 814–824. doi: 10.1016/j.ijheatmasstransfer.2017.05.008

WANG Z Z, ZHOU Z W, ZHANG D C, et al. A numerical study of flow and heat transfer characteristics of aviation kerosene in rectangular channel[J]. Journal of Air Force Engineering University (Natural Science Edition), 2019, 20(5): 22−27 (in Chinese). doi: 10.3969/j.issn.1009-3516.2019.05.004

WANG Y H, DONG M, LI S F, et al. Experimental study on heat transfer deterioration of supercritical-pressure RP-3 aviation kerosene in a vertical downward round tube[J]. Journal of Propulsion Technology, 2022, 43(6): 260−268 (in Chinese). doi: 10.13675/j.cnki.tjjs.200635

LIU Z H, SONG C Y, CHEN Q, et al. Pseudo subcooled boiling heat transfer characteristics of aviation kerosene RP-3 under super-and near-critical pressure conditions[J]. Journal of Propulsion Technology, 2021, 42(6): 1418−1424 (in Chinese). doi: 10.13675/j.cnki.tjjs.190668

LIU Y L, XU G Q, FU Y C, et al. Frictional resistance of supercritical pressure RP-3 flowing in a vertically downward tube at constant heat fluxes[J]. Chinese Journal of Aeronautics, 2022, 35(9): 117−128. doi: 10.1016/j.cja.2022.01.002

ZHU K, XU G Q, TAO Z, et al. Flow frictional resistance characteristics of kerosene RP-3 in horizontal circular tube at supercritical pressure[J]. Experimental Thermal and Fluid Science, 2013, 44: 245−252. doi: 10.1016/j.expthermflusci.2012.06.014

SUN X, MENG H, ZHENG Y. Asymmetric heating and buoyancy effects on heat transfer of hydrocarbon fuel in a horizontal square channel at supercritical pressures[J]. Aerospace Science and Technology, 2019, 93: 105358. doi: 10.1016/j.ast.2019.105358

LV L L, WEN J, FU Y C, et al. Numerical investigation on convective heat transfer of supercritical aviation kerosene in a horizontal tube under hyper gravity conditions[J]. Aerospace Science and Technology, 2020, 105: 105962. doi: 10.1016/j.ast.2020.105962

XIAO L, SU Y, QIN A, et al. Buoyancy influence on flow and heat transfer characteristics of aviation kerosene under condition of super-critical pressure[J]. Journal of Air Force Engineering University (Natural Science Edition), 2018, 19(6): 15−21 (in Chinese). doi: 10.3969/j.issn.1009-3516.2018.06.003

TAO Z, LI L W, ZHU J Q, et al. Numerical investigation on flow and heat transfer characteristics of supercritical RP-3 in inclined pipe[J]. Chinese Journal of Aeronautics, 2019, 32(8): 1885−1894. doi: 10.1016/j.cja.2019.05.007

ZHAO J J, LEI Z L, BAO Z W, et al. Pyrolysis and coking deposition of aviation kerosene under supercritical conditions in S-bend tubes[J]. Journal of Propulsion Technology, 2021, 42(3): 692−700(inChinese). doi: 10.13675/j.cnki.tjjs.190556

WANG Y H, LU Y N, LI S F, et al. Numerical study on heat transfer of supercritical-pressure RP-3 aviation kerosene in U-turn circular tubes[J]. CIESC Journal, 2021, 72(9): 4639−4648(in Chinese). doi: 10.11949/0438-1157.20201896

FENG Y, CAO J, LI X, et al. Flow and heat transfer characteristics of supercritical hydrocarbon fuel in mini channels with dimples[J]. Journal of Heat Transfer, 2017, 139(12): 122401. doi: 10.1115/1.4037086

LIU G G, LIN Y Z, LI J J, et al. Flow characteristics and phase transition of subcritical to supercritical kerosene injections in a convergent nozzle[J]. Fuel, 2023, 334: 126518. doi: 10.1016/j.fuel.2022.126518

XIAO J Y, LIN Y Z, LIU G G, et al. Flow and phase transition characteristics of supercritical RP-3 aviation kerosene in injector[J]. Journal of Propulsion Technology, 2022, 43(3): 192−200 (in Chinese).

ZHU J J, (XI/HUI) X, LIU G G, et al. Mass flow rate characteristics of sub-/ supercritical multiphase kerosene fuel nozzle[J]. Journal of Aerospace Power, 2022, 37(10): 2324−2334 (in Chinese). doi: 10.13224/j.cnki.jasp.20220271

WANG H, TAN J G. Flow characteristics of supercritical cracked kerosene based on deep learning[J]. Journal of Propulsion Technology, 2019, 40: 1419−1425. doi: 10.13675/j.cnki.tjjs.180251

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. doi: 10.1021/ef400367n

ZHENG D, YU W M, ZHONG B J. RP-3 aviation kerosene surrogate fuel and the chemical reaction kinetic model[J]. Acta Physico-Chimica Sinica, 2015, 31(4): 636−642(in Chinese). doi: 10.3866/PKU.WHXB201501231

PEI X Y, HOU L Y, MO C K, et al. Thermo-physical properties for surrogate models of aviation kerosene[J]. Journal of Aerospace Power, 2015, 30(9): 2122−2128(in Chinese). doi: 10.13224/j.cnki.jasp.2015.09.010

PEI X Y, HOU L Y. Effect of different species on physical properties for the surrogate of aviation fuel[J]. Journal of Tsinghua University(Science and Technology), 2017, 57(7): 774−779 (in Chinese) . doi: 10.16511/j.cnki.qhdxxb.2017.25.036

陶嘉伟. 亚/超临界RP-3航空煤油两组分替代物热物性分子动力学模拟研究[D]. 北京: 华北电力大学, 2022.

NARAYANASWAMY K, PITSCH H, PEPIOT P. A component library framework for deriving kinetic mechanisms for multi-component fuel surrogates: Application for jet fuel surrogates[J]. Combustion and Flame, 2016, 165: 288−309. doi: 10.1016/j.combustflame.2015.12.013

TIAN D X, LIU Y X, WANG B Y, et al. A merged kinetic mechanism study of two aviation surrogate fuels[J]. Fuel, 2021, 289: 119767. doi: 10.1016/j.fuel.2020.119767

ZHANG C H, LI B, RAO F, et al. A shock tube study of the autoignition characteristics of RP-3 jet fuel[J]. Proceedings of the Combustion Institute, 2015, 35(3): 3151−3158. doi: 10.1016/j.proci.2014.05.017

HUANG W X, CHEN F, LIU H, et al. Modeling chemical mechanism for surrogate jet fuel under scramjet operating conditions[C]// 54th AIAA Aerospace Sciences Meeting, San Diego, California, USA. AIAA, 2016: AIAA2016-0182. doi: 10.2514/6.2016-0182

YU Z Q, WEI S L, WU C C, et al. Development and verification of RP-3 aviation kerosene surrogate fuel models using a genetic algorithm[J]. Fuel, 2022, 312: 122853. doi: 10.1016/j.fuel.2021.122853

YU J, GOU X L. Comprehensive surrogate for emulating physical and kinetic properties of jet fuels[J]. Journal of Propulsion and Power, 2018, 34(3): 679−689. doi: 10.2514/1.b36766

XU J Q, GUO J J, LIU A K, et al. Construction of autoignition mechanisms for the combustion of RP-3 surrogate fuel and kinetics simulation[J]. Acta Physico-Chimica Sinica, 2015, 31(4): 643−652(inChinese). doi: 10.3866/PKU.WHXB201503022

BENSON S W, BUSS J H. Additivity rules for the estimation of molecular properties. thermodynamic properties[J]. The Journal of Chemical Physics, 1958, 29(3): 546−572. doi: 10.1063/1.1744539

WU Z Y, MAO Y B, RAZA M, et al. Surrogate fuels for RP-3 kerosene formulated by emulating molecular structures, functional groups, physical and chemical properties[J]. Combustion and Flame, 2019, 208: 388−401. doi: 10.1016/j.combustflame.2019.07.024

YAO C X, YU J. A physical surrogate fuel model for RP-3 aviation kerosene and applications[J]. Journal of Propulsion Technology, 2020, 41(4): 934−941 (in Chinese).

YU J, YU B B, YU J J. Development of comprehensive surrogate fuel model for RP-3 aviation kerosene[J]. Journal of Aerospace Power, 2020, 35(4): 673−681 (in Chinese).

SHAHSAVAN MARKADEH R, ARABKHALAJ A, BIROUK M. On the density prediction of multicomponent hydrocarbon mixtures at near- and supercritical conditions[J]. Fluid Phase Equilibria, 2022, 562: 113560. doi: 10.1016/j.fluid.2022.113560

LEACH J W, CHAPPELEAR P S, LELAND T W. Use of molecular shape factors in vapor-liquid equilibrium calculations with the corresponding states principle[J]. AIChE Journal, 1968, 14(4): 568−576. doi: 10.1002/aic.690140407

FAN X J, YU G. Analysis of thermophysical properties of Daqing RP-3 aviation kerosene[J]. Journal of Propulsion Technology, 2006, 27(2): 187−192 (in Chinese). doi: 10.3321/j.issn:1001-4055.2006.02.021

SHEN Y, LIU Y B, CAO B Y. Study on surrogate models for thermophysical properties of supercritical aviation kerosene RP-3[J]. Journal of Engineering Thermophysics, 2022, 43(4): 1048−1054(in Chinese).

TAO K H, ZHU J Q, CHENG Z Y. Calculation of thermophysical properties of supercritical RP-3 based on artificial neural network model[J]. Journal of Aerospace Power, 2023, 38(4): 806−815 (in Chinese).

GE H, FAN Y X, WANG W L, et al. Experimental study on injection characteristics of near/supercritical RP-3 aviation kerosene[J]. Journal of Aerospace Power, 2024, 39(8): 134−143(in Chinese). doi: 10.13224/j.cnki.jasp.20220614

GAO W, LIN Y Z, HUI X, et al. Injection characteristics of near critical and supercritical kerosene into quiescent atmospheric environment[J]. Fuel, 2019, 235: 775−781. doi: 10.1016/j.fuel.2018.08.048

LIANG H S, GAO W, XU Q H, et al. Injection characteristics of the supercritical jet fuel injected into the atmospheric environment[J]. Journal of Aerospace Power, 2009, 24(6): 1258−1263 (in Chinese).

FAN Z C, FAN W. Numerical simulation on effects of flow parameters on supercritical injection characteristics[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(5): 1018−1027 (in Chinese). doi: 10.7527/S1000-6893.2013.0191

JIN L, FAN W, FAN Z C, et al. Numerical investigation on effects of ambient and injection parameters on supercritical injection[J]. Journal of Aerospace Power, 2014, 29(6): 1323−1329 (in Chinese).

邢云绯, 仲峰泉, 杜蒙蒙. 超临界态煤油同轴喷射与混合特性研究[C]// 中国力学大会-2021+1论文集(第二册). 西安, 2022: 1152-1160. doi: 10.1063/1.1795011

LEE J, MADABHUSHI R, FOTACHE C, et al. Flashing flow of superheated jet fuel[J]. Proceedings of the Combustion Institute, 2009, 32(2): 3215−3222. doi: 10.1016/j.proci.2008.06.153

TANG H R, SHEN C B, DU Z B, et al. Research progress on fuel mixing enhancement technology of scramjet[J]. Aero Weaponry, 2023, 30(1): 80−94 (in Chinese). doi: 10.12132/ISSN.1673-5048.2022.0085

LIU W H, WANG X, MA W F. Surface tension effect on harmonics of Rayleigh-Taylor instability[J]. Chinese Journal of Chemical Physics, 2018, 31(1): 39−44. doi: 10.1063/1674-0068/31/cjcp1703056

LI P B, LI C Y, WANG H B, et al. Distribution characteristics and mixing mechanism of a liquid jet injected into a cavity-based supersonic combustor[J]. Aerospace Science and Technology, 2019, 94: 105401. doi: 10.1016/j.ast.2019.105401

CORN M L, COHEN J M, LEE J C, et al. Characterization of a superheated fuel jet in a crossflow[J]. Journal of Engineering for Gas Turbines and Power, 2011, 133(1): 011501. doi: 10.1115/1.4001978

YANG K, LI C Y, PAN Y, et al. Investigation of the evaporation characteristics of a transverse vaporized kerosene jet in supersonic flow[J]. Acta Astronautica, 2021, 185: 257−263. doi: 10.1016/j.actaastro.2021.04.046

LI F, WANG T Y, YANG K, et al. Effect of fuel temperature on mixing characteristics of a kerosene jet injected into a cavity-based supersonic combustor[J]. Physics of Fluids, 2023, 35(4): 043307. doi: 10.1063/5.0145494

WANG J S, LIN W, HUANG W D, et al. Numerical study on atomization and evaporation characteristics of preheated kerosene jet in a rotating detonation scramjet combustor[J]. Applied Thermal Engineering, 2022, 203: 117920. doi: 10.1016/j.applthermaleng.2021.117920

仲峰泉, 范学军, 王晶, 等. 超临界态煤油等熵流动和超声速喷注研究[C]// 第二届高超声速科技学术会议会议日程及摘要集. 黄山, 2009: 43.

FAN X J, YU G. Experiments on supersonic combustion of supercritical kerosene[J]. Journal of Propulsion Technology, 2006, 27(1): 79−82 (in Chinese). doi: 10.3321/j.issn:1001-4055.2006.01.019

QI L. Study on flame stability law of supercritical kerosene supersonic combustion[D]. Beijing: University of Chinese Academy of Sciences, 2013 (in Chinese).

RASMUSSEN C C, DRISCOLL J F, HSU K Y, et al. Stability limits of cavity-stabilized flames in supersonic flow[J]. Proceedings of the Combustion Institute, 2005, 30(2): 2825−2833. doi: 10.1016/j.proci.2004.08.185

GOLDFELD M. Specific features of ignition and flameholding of hydrocarbon fuels in high-speed flow[J]. Progress in Propulsion Physics, 2016, 8: 333−352. doi: 10.1051/eucass/201608333

POWELL O A, EDWARDS J T, NORRIS R B, et al. Development of hydrocarbon-fueled scramjet engines: The hypersonic technology (HyTech) program[J]. Journal of Propulsion and Power, 2001, 17(6): 1170−1176. doi: 10.2514/2.5891

VINCENT-RANDONNIER A, ROUXEL B, ROUX P, et al. Experimental investigations on the self-ignition of a thermally decomposed endothermic fuel in hot supersonic air flow in the MPP-LAERTE combustion test bench[C]// 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio. AIAA, 2008: AIAA 2008-2676. doi: 10.2514/6.2008-2676

王晶, 范学军, 仲峰泉, 等. 超临界煤油的亚/超声速喷注对超声速燃烧性能的影响实验研究[C]. 第二届高超声速科技学术会议会议日程及摘要集. 黄山, 2009.

YANG K, PAN Y, WANG Z G, et al. Experimental investigation of the ignition characteristics of vaporized RP-3 kerosene in supersonic flow[J]. Acta Astronautica, 2020, 174: 1−10. doi: 10.1016/j.actaastro.2020.04.022

ZHONG F Q, CHEN L H, CHANG X Y. Numerical study of ignition and combustion of partially cracked kerosene in a Mach 2.5 supersonic model combustor[C]// 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France. AIAA, 2012: AIAA 2012-5928. doi: 10.2514/6.2012-5928

YUAN Y M, YANG M, ZHANG T C, et al. Visualization of vaporized kerosene combustion in a supersonic combustor using pulsed schlieren system[C]// 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Atlanta, Georgia. 2012: AIAA 2012-3848. doi: 10.2514/6.2012-3848

ZHENG Y S, WANG S W, XIAO B G, et al. Supercritical kerosene combustion characteristics of single-head combustor[J]. Journal of Aerospace Power, 2024, 39(10): 201−210 (in Chinese).

FAN X J, YU G, LI J G, et al. Investigation of vaporized kerosene injection and combustion in a supersonic model combustor[J]. Journal of Propulsion and Power, 2006, 22(1): 103−110. doi: 10.2514/1.15427

SHIN J, SUNG H G. Combustion characteristics of hydrogen and cracked kerosene in a DLR scramjet combustor using hybrid RANS/LES method[J]. Aerospace Science and Technology, 2018, 80: 433−444. doi: 10.1016/j.ast.2018.03.006

HUANG W, DU Z B, YAN L, et al. Flame propagation and stabilization in dual-mode scramjet combustors: A survey[J]. Progress in Aerospace Sciences, 2018, 101: 13−30. doi: 10.1016/j.paerosci.2018.06.003

HANK J. Air force research laboratory hypersonic propulsion research programs[C]// 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Cincinnati, OH. AIAA, 2007: AIAA 2007-5371. doi: 10.2514/6.2007-5371

BARZEGAR G M, FALLAH K, POURMIRZAAGHA H. Characteristics of transverse hydrogen jet in presence of multi air jets within scramjet combustor[J]. Acta Astronautica, 2017, 132: 25−32. doi: 10.1016/j.actaastro.2016.11.041

PENG Y P, BARZEGAR G M, SHEIKHOLESLAMI M, et al. Mixing enhancement of the multi hydrogen fuel jets by the backward step[J]. Energy, 2020, 203: 117859. doi: 10.1016/j.energy.2020.117859

KANNAIYAN K. Computational study of the effect of cavity geometry on the supersonic mixing and combustion of ethylene[J]. Journal of Computational Science, 2020, 47: 101243. doi: 10.1016/j.jocs.2020.101243

MENGISTU Y G, MISHRA D P, HARIHARAN V. Numerical characterization of 3D nonreacting supersonic cavity combustor with inlet Mach number variation[J]. International Journal of Hydrogen Energy, 2020, 45(16): 10130−10144. doi: 10.1016/j.ijhydene.2020.01.187

YANG Y X. Study on supersonic flow pattern and flame stabilization mechanism of cavity with sudden expansion of trailing edge[D]. Changsha: National University of Defense Technology, 2018(in Chinese).

LIU H, ZHANG M Z, DOU F L. Research on strut of scramjet engine[J]. Journal of Rocket Propulsion, 2016, 42(5): 74−81 (in Chinese). doi: 10.3969/j.issn.1672-9374.2016.05.013

XUE S J, YANG A L, YANG W D, et al. Experimental investigation on kerosene supercritical combustion and flame of a coaxial injector[J]. Journal of Propulsion Technology, 2015, 36(9): 1281−1287 (in Chinese).

ZHANG T C, YUAN Y M, LI J G, et al. Characteristics of a supersonic model combustor with two-staged injections of supercritical kerosene[C]// 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Atlanta, Georgia. AIAA, 2012: AIAA 2012-3762. doi: 10.2514/6.2012-3762

ZHANG T C, WANG J, FAN X J, et al. Combustion of vaporized kerosene in supersonic model combustors with dislocated dual cavities[J]. Journal of Propulsion and Power, 2014, 30(5): 1152−1160. doi: 10.2514/1.b35096

FAN X J, YU G, LI J G, et al. Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance[J]. Combustion Science and Technology, 2007, 179(10): 2199−2217. doi: 10.1080/00102200701386198

FAN X J, YU G, LI J G, et al. Performances of supersonic model combustors with distributed injection of supercritical kerosene[C]// 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Cincinnati, OH. AIAA, 2007: AIAA 2007-5406. doi: 10.2514/6.2007-5406

YU G, FAN X J, LI J G, et al. Experimental study on combustion of thermally-cracked kerosene in model supersonic combustors[C]// 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Sacramento, California. 2006: AIAA 2006-4514. doi: 10.2514/6.2006-4514

SUN M B, ZHONG Z, LIANG J H, et al. Experimental investigation of supersonic model combustor with distributed injection of supercritical kerosene[J]. Journal of Propulsion and Power, 2014, 30(6): 1537−1542. doi: 10.2514/1.b35169

XU C Q, HE G Q, QIN F, et al. Research on ramjet-mode combustion organization by using vaporized kerosene injection in RBCC combustor[J]. Journal of Propulsion Technology, 2014, 35(4): 507−513 (in Chinese).

范学军, 仲峰泉, 王晶, 等. 双路喷注超临界态煤油的超燃特性研究[C]// 第一届高超声速科技学术会议. 丽江, 2008: 179-185.

ZHANG T C, WANG J, QI L, et al. Blowout limits of cavity-stabilized flame of supercritical kerosene in supersonic combustors[J]. Journal of Propulsion and Power, 2014, 30(5): 1161−1166. doi: 10.2514/1.b35120

ZHANG T C, WANG J, QI L, et al. Blowout limits of supercritical kerosene in supersonic combustors[C]// 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, 2013: AIAA 2013-3696. doi: 10.2514/6.2013-3696

王晶, 范学军, 李建国, 等. 航空煤油超声速稳定燃烧贫富油极限实验研究[C]// 第三届高超声速科技学术会议会议文集. 无锡, 2010: 267-272.

齐力, 张泰昌, 范学军. 超声速燃烧稳燃极限的理论研究[C]//第七届全国流体力学学术会议论文摘要集. 桂林, 2012: 242.