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第 46 卷             吴    宇,等: 进口压力扰动对氢气燃料旋转爆轰特性的影响                               第 9 期

                    ijheatmasstransfer.2023.125081.
               [17]   ANAND V, ST. GEORGE A, GUTMARK E. Amplitude modulated instability in reactants plenum of a rotating detonation
                    combustor [J]. International Journal of Hydrogen Energy, 2017, 42(17): 12629–12644. DOI: 10.1016/j.ijhydene.2017.03.218.
               [18]   FROLOV S M, ZVEGINTSEV V I, IVANOV V S, et al. Hydrogen-fueled detonation ramjet model: wind tunnel tests at
                    approach air stream Mach number 5.7 and stagnation temperature 1500 K [J]. International Journal of Hydrogen Energy, 2018,
                    43(15): 7515–7524. DOI: 10.1016/j.ijhydene.2018.02.187.
               [19]   WEN H C, XIE Q F, WANG B. Propagation behaviors of rotating detonation in an obround combustor [J]. Combustion and
                    Flame, 2019, 210: 389–398. DOI: 10.1016/j.combustflame.2019.09.008.
               [20]   XIA Z J, MA H, LIU C, et al. Experimental investigation on the propagation mode of rotating detonation wave in plane-radial
                    combustor [J]. Experimental Thermal and Fluid Science, 2019, 103: 364–376. DOI: 10.1016/j.expthermflusci.2019.01.032.
               [21]   SOSA J, BURKE R, AHMED K A, et al. Experimental evidence of H 2 /O 2  propellants powered rotating detonation waves [J].
                    Combustion and Flame, 2020, 214: 136–138. DOI: 10.1016/j.combustflame.2019.12.031.
               [22]   ZHOU S B, MA H, ZHOU C S, et al. Experimental research on the propagation process of rotating detonation wave with a
                    gaseous hydrocarbon mixture fuel [J]. Acta Astronautica, 2021, 179: 1–10. DOI: 10.1016/j.actaastro.2020.10.027.
               [23]   BAI Q D, HAN J X, ZHANG S J, et al. Experimental study on the auto-initiation of rotating detonation with high-temperature
                    hydrogen-rich gas [J]. Physics of Fluids, 2023, 35(4): 045121. DOI: 10.1063/5.0144322.
               [24]   WU Y W, GUO J X, XU G, et al. Wave mode observation of hydrogen/oxygen driven rotating detonations in the hollow and
                    annular rotating detonation rocket engine [J]. Physics of Fluids, 2024, 36(11): 115105. DOI: 10.1063/5.0237542.
               [25]   WANG J P, HAN J X, BAI Q D, et al. Experimental study on rotating detonation characteristics and multiple waves evolution
                    mechanisms in CH 4 /CO/H 2  gas mixtures [J]. International Journal of Hydrogen Energy, 2025, 115: 101–112. DOI: 10.1016/j.
                    ijhydene.2025.03.071.
               [26]   ZHENG H T, MENG Q Y, ZHAO N B, et al. Numerical investigation on H 2 /air non-premixed rotating detonation engine
                    under different equivalence ratios [J]. International Journal of Hydrogen Energy, 2020, 45(3): 2289–2307. DOI: 10.1016/j.
                    ijhydene.2019.11.014.
               [27]   ZHAO M J, ZHANG H W. Origin and chaotic propagation of multiple rotating detonation waves in hydrogen/air mixtures [J].
                    Fuel, 2020, 275: 117986. DOI: 10.1016/j.fuel.2020.117986.
               [28]   YAO K P, YANG P F, TENG H H, et al. Effects of injection parameters on propagation patterns of hydrogen-fueled rotating
                    detonation  waves  [J].  International  Journal  of  Hydrogen  Energy,  2022,  47(91):  38811–38822.  DOI:  10.1016/j.ijhydene.
                    2022.09.051.
               [29]   CHEN H W, SI C W, WU Y, et al. Numerical investigation of the effect of equivalence ratio on the propagation characteristics
                    and performance of rotating detonation engine [J]. International Journal of Hydrogen Energy, 2023, 48(62): 24074–24088.
                    DOI: 10.1016/j.ijhydene.2023.03.190.
               [30]   WANG  F,  LIU  Q  Y,  WENG  C  S.  On  the  feasibility  and  performance  of  the  ammonia/hydrogen/air  rotating  detonation
                    engines [J]. Physics of Fluids, 2023, 35(6): 066133. DOI: 10.1063/5.0152609.
               [31]   HU  J  H,  ZHANG  B.  Time/frequency  domain  analysis  of  detonation  wave  propagation  mechanism  in  a  linear  rotating
                    detonation combustor [J]. Applied Thermal Engineering, 2024, 255: 124014. DOI: 10.1016/j.applthermaleng.2024.124014.
               [32]   XIONG A, DANG Y T, ZHANG Y Z, et al. Study on the combustion characteristics of high-speed non-premixed reactants
                    enhanced  by  rotating  detonation  jet  [J].  Aerospace  Science  and  Technology,  2025,  162:  110207.  DOI:  10.1016/j.ast.2025.
                    110207.
               [33]   CHEN  H  W,  SI  C  W,  HU  H  B,  et  al.  Effects  of  the  perturbation  inlet  on  the  evolution  and  oscillation  characteristics  of
                    multiple  rotating  detonation  waves  [J].  Aerospace  Science  and  Technology,  2023,  141:  108586.  DOI:  10.1016/j.ast.2023.
                    108586.
               [34]   ZHANG X J, WANG Y N, CHENG M, et al. Numerical research on the propagation characteristics and evolution mechanisms
                    of rotating detonation waves with the spatial fluctuation of inlet total pressure [J]. Physics of Fluids, 2024, 36(9): 096122.
                    DOI: 10.1063/5.0226308.
               [35]   WANG Y N, ZHANG X J, LIU P L, et al. Effect of the inlet spatial fluctuation on the gas-solid continuous rotating detonation
                    flow field characteristics [J]. Physics of Fluids, 2024, 36(7): 076107. DOI: 10.1063/5.0215308.
               [36]   YAO S, HAN X, LIU Y, et al. Numerical study of rotating detonation engine with an array of injection holes [J]. Shock
                    Waves, 2017, 27(3): 467–476. DOI: 10.1007/s00193-016-0692-6.


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