CURRAN E T. Scramjet engines:the first forty years[J]. Journal of Propulsion and Power, 2001, 17(6):1138-1148. https://doi.org/10.2514/2.5875

WANG Z G, SUN M B, WANG H B, et al. Mixing-related low frequency oscillation of combustion in an ethylene-fueled supersonic combustor[J]. Proceedings of the Combustion Institute, 2015, 35(2):2137-2144. https://doi.org/10.1016/j.proci.2014.09.005

GOYNE C, HALL C, O'BRIEN W, et al. The hy-V scramjet flight experiment[C ] //14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, Canberra, Australia. Reston, Virigina: AIAA. AIAA 2006-7901. https://doi.org/10.2514/6.2006-7901

STAMP G, GHOSH A, ZANG A, et al. Experimental characterization of acoustic wave propagation in a supersonic duct[C ] //41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Tucson, Arizona. Reston, Virigina: AIAA. AIAA 2005-4144. https://doi.org/10.2514/6.2005-4144

LIN K C, TAM C J, BOXX I, et al. Flame characteristics and fuel entrainment inside a cavity flame holder of a scramjet combustor[C ] //43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Cincinnati, OH. Reston, Virigina: AIAA. AIAA 2007-5381. https://doi.org/10.2514/6.2007-5381

FROST M A, GANGURDE D Y, PAULL A, et al. Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow[J]. AIAA Journal, 2009, 47(4):1050-1053. https://doi.org/10.2514/1.40868

REIJASSE P, CORBEL B, SOULEVANT D. Unsteadiness and asymmetry of shock-induced separation in a planar two-dimensional nozzle: A flow description[C ] //30th Fluid Dynamics Conference, Norfolk, VA, USA. Reston, Virigina: AIAA. AIAA 99-3694. https://doi.org/10.2514/6.1999-3694

CLEMENS N T, NARAYANASWAMY V. Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions[J]. Annual Review of Fluid Mechanics, 2014, 46(1):469-492. https://doi.org/10.1146/annurev-fluid-010313-141346

CAI Z, WANG T Y, SUN M B. Review of cavity ignition in supersonic flows[J]. Acta Astronautica, 2019, 165:268-286. https://doi.org/10.1016/j.actaastro.2019.09.016

WANG Y N, WANG Z G, SUN M B, et al. Effects of auto-ignition on combustion characteristics in a hydrogen-fueled dual-mode scramjet combustor[J]. Acta Astronautica, 2018, 153:154-158. https://doi.org/10.1016/j.actaastro.2018.10.013

KIM C H, JEUNG I S, CHOI B, et al. Flowfield characteristics of a hypermixer interacting with transverse injection in supersonic flow[J]. AIAA Journal, 2012, 50(8):1742-1753. https://doi.org/10.2514/1.j051588

LIU B, HE G Q, QIN F. Simulation of supersonic Ethylene-Hydrogen and air auto-ignition flame using skeletal mechanism[J]. Acta Astronautica, 2018, 152:521-533. https://doi.org/10.1016/j.actaastro.2018.08.046

VINOGRADOV V A, SHIKHMAN Y M, SEGAL C. A review of fuel pre-injection in supersonic, chemically reacting flows[J]. Applied Mechanics Reviews, 2007, 60(4):139-148. https://doi.org/10.1115/1.2750346

FOTIA M L, DRISCOLL J F. Ram-scram transition and flame/shock-train interactions in a model scramjet experiment[J]. Journal of Propulsion and Power, 2013, 29(1):261-273. https://doi.org/10.2514/1.b34486

AN B, WANG Z G, YANG L C, et al. Experimental investigation on the impacts of ignition energy and position on ignition processes in supersonic flows by laser induced plasma[J]. Acta Astronautica, 2017, 137:444-449. https://doi.org/10.1016/j.actaastro.2017.05.013

TUTTLE S G, CARTER C D, HSU K Y. Particle image velocimetry in a nonreacting and reacting high-speed cavity[J]. Journal of Propulsion and Power, 2014, 30(3):576-591. https://doi.org/10.2514/1.b34974

GRUBER M R, DONBAR J M, CARTER C D, et al. Mixing and combustion studies using cavity-based flameholders in a supersonic flow[J]. Journal of Propulsion and Power, 2004, 20(5):769-778. https://doi.org/10.2514/1.5360

DRISCOLL J F, RASMUSSEN C C. Correlation and analysis of blowout limits of flames in high-speed airflows[J]. Journal of Propulsion and Power, 2005, 21(6):1035-1044. https://doi.org/10.2514/1.13329

WANG Z G. Internal combustion processes of liquid rocket engines. Beijing:National Defence Industrial Press. 2012. (in Chinese) ISBN:9787118085259

汪洪波.超声速气流中凹腔稳定的射流燃烧模式及振荡机制研究[D].长沙: 国防科技大学; 2012.

HELLER H H, BLISS D B. The physical mechanism of flow-induced pressure fluctuations in cavities and concepts for their suppression[C ] //2nd Aeroacoustics Conference, Hampton, VA, USA. Reston, Virigina: AIAA. AIAA 75-491. https://doi.org/10.2514/6.1975-491

Rossiter J E. Wind tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds[R]. Ministry of Aviation; Royal Aircraft Establishment; RAE Farnborough. RAE 64037, 1964.

CHOI J Y, MA F H, YANG V. Combustion oscillations in a scramjet engine combustor with transverse fuel injection[J]. Proceedings of the Combustion Institute, 2005, 30(2):2851-2858. https://doi.org/10.1016/j.proci.2004.08.250

CHOI J Y, MA F H, YANG V, et al. Detached eddy simulation of combustion dynamics in scramjet combustors[C ] //43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Cincinnati, OH. Reston, Virigina: AIAA. AIAA 2007-5027. https://doi.org/10.2514/6.2007-5027

CHOI J, GHODKE C, MENON S. Large-eddy simulation of cavity flame-holding in a Mach 2.5 cross flow[C ] //48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virigina: AIAA. AIAA 2010-414. https://doi.org/10.2514/6.2010-414

WON S H, JEUNG I S, CHOI J Y. DES modeling of supersonic combustion in scramjet combustors[C ] //42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Sacramento, California. Reston, Virigina: AIAA. AIAA 2006-5097. https://doi.org/10.2514/6.2006-5097

WANG H B, SUN M B, QIN N, et al. Characteristics of oscillations in supersonic open cavity flows[J]. Flow, Turbulence and Combustion, 2013, 90(1):121-142. https://doi.org/10.1007/s10494-012-9434-8

WANG H B, WANG Z G, SUN M B, et al. Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder[J]. Proceedings of the Combustion Institute, 2013, 34(2):2073-2082. https://doi.org/10.1016/j.proci.2012.06.049

WANG H B, WANG Z G, SUN M B, et al. Large-Eddy/Reynolds-averaged Navier-Stokes simulation of combustion oscillations in a cavity-based supersonic combustor[J]. International Journal of Hydrogen Energy, 2013, 38(14):5918-5927. https://doi.org/10.1016/j.ijhydene.2013.02.100

WANG H B, WANG Z G, SUN M B. Experimental study of oscillations in a scramjet combustor with cavity flameholders[J]. Experimental Thermal and Fluid Science, 2013, 45:259-263. https://doi.org/10.1016/j.expthermflusci.2012.10.013

TIAN X D, CHEN L H, GU H B, et al. Experimental study of combustion oscillations in a dual-mode scramjet[C ] //20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland. Reston, Virginia: AIAA. AIAA 2015-3587. https://doi.org/10.2514/6.2015-3587

田旭东.超声速燃烧振荡特性实验研究[D].北京: 中国科学院大学, 2015.

FLEIFIL M. Response of a laminar premixed flame to flow oscillations:a kinematic model and thermoacoustic instability results[J]. Combustion and Flame, 1996, 106(4):487-510. https://doi.org/10.1016/0010-2180(96)00049-1

OUYANG H, LIU W D, SUN M B. The influence of cavity parameters on the combustion oscillation in a single-side expansion scramjet combustor[J]. Acta Astronautica, 2017, 137:52-59. https://doi.org/10.1016/j.actaastro.2017.03.018

MA F H, LI J, YANG V, et al. Thermoacoustic flow instability in a scramjet combustor[C ] //41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Tucson, Arizona. Reston, Virigina: AIAA. AIAA 2005-3824. https://doi.org/10.2514/6.2005-3824

LI J, MA F H, YANG V, et al. A comprehensive study of ignition transient in an ethylene-fueled scramjet combustor[C ] //43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Cincinnati, OH. Reston, Virigina: AIAA. AIAA 2007-5025. https://doi.org/10.2514/6.2007-5025

LIN K C, JACKSON K, BEHDADNIA R, et al. Acoustic characterization of an ethylene-fueled scramjet combustor with a rectangular cavity flameholder[C ] //43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Cincinnati, OH. Reston, Virigina: AIAA. AIAA 2007-5382. https://doi.org/10.2514/6.2007-5382

LIN K C, JACKSON K, BEHDADNIA R, et al. Acoustic characterization of an ethylene-fueled scramjet combustor with a cavity flameholder[J]. Journal of Propulsion and Power, 2010, 26(6):1161-1170. https://doi.org/10.2514/1.43338

CUI X D. Investigations on low frequency combustion oscillations in supersonic flow[D]. Changsha: National University of Defense Technology, 2014. (in Chinese)

KNIGHT D, YAN H, PANARAS A G, et al. Advances in CFD prediction of shock wave turbulent boundary layer interactions[J]. Progress in Aerospace Sciences, 2003, 39(2/3):121-184. https://doi.org/10.1016/s0376-0421(02)00069-6

DOLLING D S. Fifty years of shock-wave/boundary-layer interaction research:What next?[J]. AIAA Journal, 2001, 39(8):1517-1531. https://doi.org/10.2514/2.1476

PIPONNIAU S, DUSSAUGEJ P, DEBIÈVE J F, et al. A simple model for low-frequency unsteadiness in shock-induced separation[J]. Journal of Fluid Mechanics, 2009, 629:87-108. https://doi.org/10.1017/s0022112009006417

KOO H, RAMAN V. Large-eddy simulation of a supersonic inlet-isolator[J]. AIAA Journal, 2012, 50(7):1596-1613. https://doi.org/10.2514/1.j051568

DO H, IM S K, MUNGAL M G, et al. The influence of boundary layers on supersonic inlet flow unstart induced by mass injection[J]. Experiments in Fluids, 2011, 51(3):679-691. https://doi.org/10.1007/s00348-011-1077-3

GEERTS J S, YU K H. Experimental characterization of isolator shock train propagation[C ] //18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France. Reston, Virigina: AIAA. AIAA 2012-5891. https://doi.org/10.2514/6.2012-5891

GEERTS J S, YU K H. Visualization of shock train-boundary layer interaction in Mach 2.5 isolator flow[C ] //43rd Fluid Dynamics Conference, San Diego, CA. Reston, Virginia: AIAA. AIAA 2013-3102. https://doi.org/10.2514/6.2013-3102

BRUCE P J K, BABINSKY H, TARTINVILLE B, et al. Corner effect and asymmetry in transonic channel flows[J]. AIAA Journal, 2011, 49(11):2382-2392. https://doi.org/10.2514/1.j050497

SU W Y, ZHANG K Y. Back-pressure effects on the hypersonic inlet-isolator pseudoshock motions[J]. Journal of Propulsion and Power, 2013, 29(6):1391-1399. https://doi.org/10.2514/1.b34803

SU W Y, JI Y X, CHEN Y. Effects of dynamic backpressure on pseudoshock oscillations in scramjet inlet-isolator[J]. Journal of Propulsion and Power, 2016, 32(2):516-528. https://doi.org/10.2514/1.b35898

LI N, CHANG J T, XU K J, et al. Oscillation of the shock train in an isolator with incident shocks[J]. Physics of Fluids, 2018, 30(11):116102. https://doi.org/10.1063/1.5053451

XIONG B, WANG Z G, FAN X Q, et al. Response of shock train to high-frequency fluctuating backpressure in an isolator[J]. Journal of Propulsion and Power, 2017, 33(6):1520-1528. https://doi.org/10.2514/1.b36291

OLSON B J, LELE S K. Large-Eddy Simulation of an over-expanded planar nozzle[C ] //41st AIAA Fluid Dynamics Conference and Exhibit, Honolulu, Hawaii. Reston, Virigina: AIAA.. AIAA 2011-3908. https://doi.org/10.2514/6.2011-3908

YU Y, XU J L, MO J W, et al. Principal parameters in flow separation patterns of over-expanded single expansion RAMP nozzle[J]. Engineering Applications of Computational Fluid Mechanics, 2014, 8(2):274-288. https://doi.org/10.1080/19942060.2014.11015513

YU Y, XU J, YU K, et al. Unsteady transitions of separation patterns in single expansion ramp nozzle[J]. Shock Waves, 2015, 25(6):623-633. https://doi.org/10.1007/s00193-015-0595-y

PAPAMOSCHOU D, ZILL A. Fundamental investigation of supersonic nozzle flow separation[C ] //42n d AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA. AIAA 2004-1111. https://doi.org/10.2514/6.2004-1111

PAPAMOSCHOU D, JOHNSON A. Unsteady phenomena in supersonic nozzle flow separation[C ] //36th AIAA Fluid Dynamics Conference and Exhibit, San Francisco, California. Reston, Virigina: AIAA.. AIAA 2006-3360. https://doi.org/10.2514/6.2006-3360

XIAO Q, TSAI H M, PAPAMOSCHOU D. Numerical investigation of supersonic nozzle flow separation[J]. AIAA Journal, 2007, 45(3):532-541. https://doi.org/10.2514/1.20073

JOHNSON A D, PAPAMOSCHOU D. Instability of shock-induced nozzle flow separation[J]. Physics of Fluids, 2010, 22(1):016102. https://doi.org/10.1063/1.3278523

OLSON B, LELE S. Low frequency unsteadiness in nozzle flow separation[C ] //42nd AIAA Fluid Dynamics Conference and Exhibit, New Orleans, Louisiana. Reston, Virigina: AIAA. AIAA 2012-2974. https://doi.org/10.2514/6.2012-2974

LAURENCE S J, LIEBER D, MARTINEZ SCHRAMM J, et al. Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part I: Shock-tunnel experiments[J ] . Combustion and Flame, 2015, 162(4): 921-931. https://doi.org/10.1016/j.combustflame.2014.09.016

YUAN Y M, ZHANG T C, YAO W, et al. Study on flame stabilization in a dual-mode combustor using optical measurements[J]. Journal of Propulsion and Power, 2015, 31(6):1524-1531. https://doi.org/10.2514/1.b35689

SUN M B, ZHONG Z, GAO T Y, et al. Asymmetric combustion characteristics of transverse ethylene injection in a rectangular supersonic combustor with single-side expansion[C]//21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China. Reston, Virginia: AIAA. AIAA 2017-2233. https: //doi.org/10.2514/6.2017-2233

GAO T Y, LIANG J H, SUN M B, et al. Dynamic combustion characteristics in a rectangular supersonic combustor with single-side expansion[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2017, 231(10):1862-1872. https://doi.org/10.1177/0954410016662062

GAO T Y, LIANG J H, SUN M B. Decoupling analysis on oscillation of separated region in a supersonic combustor with single-side expansion[J]. Journal of Propulsion Technology, 2018, 39(10):2381-2393. (in Chinese)

GAO T Y, LIANG J H, SUN M B, et al. Analysis of separation modes variation in a scramjet combustor with single-side expansion[J]. AIAA Journal, 2017, 55(4):1307-1317. https://doi.org/10.2514/1.j055411

GAO T Y, LIANG J H, SUN M B. Symmetric/asymmetric separation transition in a supersonic combustor with single-side expansion[J]. Physics of Fluids, 2017, 29(12):126102. https://doi.org/10.1063/1.4990668

SUN M B, GONG C, ZHANG S P, et al. Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition[J]. Experimental Thermal and Fluid Science, 2012, 43:90-96. https://doi.org/10.1016/j.expthermflusci.2012.03.028

XI W X, WANG Z G, SUN M B, et al. Experimental investigation of ignition transient phase in model supersonic combustor[J]. Journal of Aerospace Engineering, 2014, 27(4):04014009. https://doi.org/10.1061/(asce)as.1943-5525.0000334

OMBRELLO T, CARTER C, MCCALL J, et al. Enhanced mixing in supersonic flow using a pulse detonator[J]. Journal of Propulsion and Power, 2015, 31(2):654-663. https://doi.org/10.2514/1.b35316

OMBRELLO T, CARTER C D, TAM C J, et al. Cavity ignition in supersonic flow by pulse detonation[C ] //52nd Aerospace Sciences Meeting, National Harbor, Maryland. Reston, Virginia: AIAA. AIAA 2014-0286. https://doi.org/10.2514/6.2014-0286

LEONOV S B. Electrically driven supersonic combustion[J]. Energies, 2018, 11(7):1733. https://doi.org/10.3390/en11071733

JU Y G, SUN W T. Plasma assisted combustion:Dynamics and chemistry[J]. Progress in Energy and Combustion Science, 2015, 48:21-83. https://doi.org/10.1016/j.pecs.2014.12.002

FRIDMAN A, NESTER S, KENNEDY L A, et al. Gliding arc gas discharge[J]. Progress in Energy and Combustion Science, 1999, 25(2):211-231. https://doi.org/10.1016/s0360-1285(98)00021-5

LEONOV S, YARANTSEV D, NAPARTOVICH A, et al. Plasma-assisted ignition and flameholding in high-speed flow[C ] //44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA. AIAA 2006-563. https://doi.org/10.2514/6.2006-563

PHUOC T X. Laser-induced spark ignition fundamental and applications[J]. Optics and Lasers in Engineering, 2006, 44(5):351-397. https://doi.org/10.1016/j.optlaseng.2005.03.008

孙英英.碳氢燃料超燃火焰传播与性能的实验研究[D].合肥: 中国科学技术大学, 2000.

MICKA D, DRISCOLL J. Reaction zone imaging in a dual-mode scramjet combustor using CH-PLIF[C ] //44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Hartford, CT. Reston, Virigina: AIAA. AIAA 2008-5071. https://doi.org/10.2514/6.2008-5071

MICKA D J, DRISCOLL J F. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder[J]. Proceedings of the Combustion Institute, 2009, 32(2):2397-2404. https://doi.org/10.1016/j.proci.2008.06.192

MICKA D, TORREZ S, DRISCOLL J. Heat release distribution in a dual-mode scramjet combustor - measurements and modeling[C ] //16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany. Reston, Virigina: AIAA. AIAA 2009-7362. https://doi.org/10.2514/6.2009-7362

MICKA D, DRISCOLL J. Dual-mode combustion of a jet in cross-flow with cavity flameholder[C ] //46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA. AIAA 2008-1062. https://doi.org/10.2514/6.2008-1062

NOH J, CHOI J Y, BYUN J R, et al. Numerical study of the auto-ignition of ethylene in an scramjet combustor with air throttling[C ] //46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Nashville, TN. Reston, Virigina: AIAA. AIAA 2010-7036. https://doi.org/10.2514/6.2010-7036

LIU B, AN J, QIN F, et al. Numerical investigation of the auto-ignition of transient hydrogen injection in supersonic airflow[J]. International Journal of Hydrogen Energy, 2019, 44(45):25042-25053. https://doi.org/10.1016/j.ijhydene.2019.07.215

MILLER J D, PELTIER S J, SLIPCHENKO M N, et al. Investigation of transient ignition processes in a model scramjet pilot cavity using simultaneous 100kHz formaldehyde planar laser-induced fluorescence and CH * chemiluminescence imaging[J ] . Proceedings of the Combustion Institute, 2017, 36(2):2865-2872. https://doi.org/10.1016/j.proci.2016.07.060

BARNES F W, SEGAL C. Cavity-based flameholding for chemically-reacting supersonic flows[J]. Progress in Aerospace Sciences, 2015, 76:24-41. https://doi.org/10.1016/j.paerosci.2015.04.002

CAI Z, ZHU J J, SUN M B, et al. Laser-induced plasma ignition in a cavity-based scramjet combustor[J]. AIAA Journal, 2018, 56(12):4884-4892. https://doi.org/10.2514/1.j057081

CAI Z, ZHU J J, SUN M B, et al. Ignition processes and modes excited by laser-induced plasma in a cavity-based supersonic combustor[J]. Applied Energy, 2018, 228:1777-1782. https://doi.org/10.1016/j.apenergy.2018.07.079

赵国焱.超声速气流中火焰闪回诱发与火焰传播机制研究[D].长沙: 国防科技大学, 2019.

SUN M B, CUI X D, WANG H B, et al. Flame flashback in a supersonic combustor fueled by ethylene with cavity flameholder[J]. Journal of Propulsion and Power, 2015, 31(3):976-981. https://doi.org/10.2514/1.b35580

HUANG Z W, HE G Q, QIN F, et al. Combustion oscillation study in a kerosene fueled rocket-based combined-cycle engine combustor[J]. Acta Astronautica, 2016, 129:260-270. https://doi.org/10.1016/j.actaastro.2016.09.024

MATHUR T, GRUBER M, JACKSON K, et al. Supersonic combustion experiments with a cavity-based fuel injector[J]. Journal of Propulsion and Power, 2001, 17(6):1305-1312. https://arc.aiaa.org/doi/abs/10.2514/2.5879

LI D P, DING M, LIANG J H, et al. Ignition experimental for liquid hydrocarbon fueled scramiet with simulated flight Mach 4[J]. Journal of Propulsion Technology, 2009, 30(4):385-389, 395. (in Chinese)

TIAN Y, YANG S H, LE J L, et al. Investigation of combustion process of a kerosene fueled combustor with air throttling[J]. Combustion and Flame, 2017, 179:74-85. https://doi.org/10.1016/j.combustflame.2017.01.021

李大鹏.煤油双模态冲压发动机燃烧室工作过程研究[D]. : 长沙: 国防科技大学, 2006.

ZHAO G Y, SUN M B, WU J S, et al. Investigation of flame flashback phenomenon in a supersonic crossflow with ethylene injection upstream of cavity flameholder[J]. Aerospace Science and Technology, 2019, 87:190-206. https://doi.org/10.1016/j.ast.2019.02.018

LAURENCE S J, KARL S, MARTINEZ SCHRAMM J, et al. Transient fluid-combustion phenomena in a model scramjet[J]. Journal of Fluid Mechanics, 2013, 722:85-120. https://doi.org/10.1017/jfm.2013.56

LIU Q L, BACCARELLA D, MCGANN B, et al. Cavity-enhanced combustion stability in an axisymmetric scramjet model[J]. AIAA Journal, 2019, 57(9):3898-3909. https://doi.org/10.2514/1.j058204

ZHAO G Y, SUN M B, WANG Y N, et al. Investigations of injection parameters on combustion oscillation in a supersonic crossflow[J]. Acta Astronautica, 2018, 152:426-436. https://doi.org/10.1016/j.actaastro.2018.08.041

BEN-YAKAR A, HANSON R K. Cavity flame-holders for ignition and flame stabilization in scramjets:an overview[J]. Journal of Propulsion and Power, 2001, 17(4):869-877. https://doi.org/10.2514/2.5818

丁猛.基于凹腔的超声速燃烧火焰稳定技术研究[D].长沙: 国防科技大学, 2005.

MITANI T, IZUMIKAWA M. Criteria for flame holding in H2-fueled scramjet engines[J]. Proceedings of the Combustion Institute, 2000, 28(1):689-695. https://doi.org/10.1016/S0082-0784(00)80270-2

DRISCOLL J F, RASMUSSEN C C. Correlation and analysis of blowout limits of flames in high-speed airflows[J]. Journal of Propulsion and Power, 2005, 21(6):1035-1044. https://doi.org/10.2514/1.13329

RASMUSSEN C, DRISCOLL J. Blowout limits of flames in high-speed airflows: critical damkohler number[C ] //44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Hartford, CT. Reston, Virigina: AIAA. AIAA 2008-4571. https://doi.org/10.2514/6.2008-4571

LE J L, YANG S H, LI H B. Analysis and correlation of flame stability limits in supersonic flow with cavity flameholder[C ] //18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France. Reston, Virigina: AIAA. AIAA 2012-5948. https://doi.org/10.2514/6.2012-5948

WANG Z G, YANG Y X, LIANG J H, et al. Analysis and modeling of blowout limits of cavity flame in supersonic flows[J]. Scientia Sinica(Technologica), 2014, 44(9):961-972. (in Chinese)

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. https://doi.org/10.2514/1.b35120

RETAUREAU G, MENON S. Experimental studies on flame stability of a fueled cavity in a supersonic crossflow[C ] //46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Nashville, TN. Reston, Virigina: AIAA. AIAA 2010-6718. https://doi.org/10.2514/6.2010-6718

SONG X L, WANG H B, SUN M B, et al. Mixing and combustion characteristics in a cavity-based supersonic combustor with different injection schemes[J]. Acta Astronautica, 2019, 159:584-592. https://doi.org/10.1016/j.actaastro.2019.02.012

LIN K C, TAM C J, JACKSON K. Study on the operability of cavity flameholders inside a scramjet combustor[C ] //45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Denver, Colorado. Reston, Virigina: AIAA. AIAA 2007-5381. https://doi.org/10.2514/6.2009-5028

GHODKE C, RETAUREAU G, CHOI J, et al. Numerical and experimental studies of flame stability in a cavity stabilized hydrocarbon-fueled scramjet[C ] //17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, California. Reston, Virigina: AIAA. AIAA 2011-2365. https://doi.org/10.2514/6.2011-2365

ALLEN W, KING P, GRUBER M, et al. Fuel-air injection effects on combustion in cavity-based flameholders in a supersonic flow[C ] //41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit, Tucson, Arizona. Reston, Virigina: AIAA. AIAA 2005-4105. https://doi.org/10.2514/6.2005-4105

HAMMACK S D, LEE T, HSU K Y, et al. High-repetition-rate OH planar laser-induced fluorescence of a cavity flameholder[J]. Journal of Propulsion and Power, 2013, 29(5):1248-1251. https://doi.org/10.2514/1.b34756

ALLISON P, FREDERICKSON K, KIRIK J W, et al. Investigation of flame structure and combustion dynamics using CH 2 O PLIF and high-speed CH chemiluminescence in a premixed dual-mode scramjet combustor[C ] //54th AIAA Aerospace Sciences Meeting, San Diego, California, USA. Reston, Virginia: AIAA. AIAA 2016-0441. https://doi.org/10.2514/6.2016-0441

SONG X L, WANG H B, SUN M B, et al. Experimental study of near-blowoff characteristics in a cavity-based supersonic combustor[J]. Acta Astronautica, 2018, 151:37-43. https://doi.org/10.1016/j.actaastro.2018.05.048

WANG H B, LI P B, ZHANG Y X, et al. Numerical study on near-blowoff characteristics of cavity-stabilized premixed flames in supersonic flows[C ] //21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China. Reston, Virginia: AIAA. AIAA 2017-2160. https://doi.org/10.2514/6.2017-2160