Page 18 - 《爆炸与冲击》2023年第2期

第 43 卷 杨 帆，等： 煤油液滴直径对两相旋转爆轰发动机流场的影响 第 2 期

[27] SARACOGLU, BAYINDIR H, et al. Unsteady performance of rotating detonation engines with different exhaust nozzles [J].
Journal of Propulsion and Power, 2017, 33(1): 1–10. DOI: 10.2514/1.B36164.
[28] KAILASANATH K. Liquid-fueled detonations in tubes [J]. Journal of Propulsion and Power, 2006, 22(6): 1261–1268. DOI:
10.2514/1.19624.
[29] SCHWER D A. Multi-dimensional simulations of liquid-fueled JP-10/oxygen detonations [C] // AIAA Propulsion and Energy
Forum. Indianapolis, USA: AIAA, 2019. DOI: 10.2514/6.2019-4042.
[30] BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of a heterogeneous kerosene-air mixture
with addition of hydrogen [J]. Combustion, Explosion, and Shock Waves, 2016, 52(3): 371–373. DOI: 10.1134/S0010508216
030187.
[31] ZHENG Q, MENG H L, WENG C S, et al. Experimental research on the instability propagation characteristics of liquid
kerosene rotating detonation wave [J]. Defence Technology, 2020, 16(6): 1106–1115. DOI: 10.1016/j.dt.2020.06.028.
[32] LI J M, CHANG P H, LI L, et al. Investigation of injection strategy for liquid-fuel rotating detonation engine [C] // AIAA
Aerospace Sciences Meeting. Kissimmee, Florida, USA: AIAA, 2018. DOI: 10.2514/6.2018-0403.
[33] MENG Q Y, ZHAO M J, ZHENG H T, et al. Eulerian-Lagrangian modelling of rotating detonative combustion in partially
pre-vaporized n-heptane sprays with hydrogen addition [J]. Fuel, 2021, 290: 119808. DOI: 10.1016/j.fuel.2020.119808.
[34] 徐高, 翁春生, 康楠, 等. 考虑燃料雾化的气液两相连续旋转爆轰数值模拟 [J]. 推进技术, 2022, 43(1): 200249. DOI:
10.13675/j.cnki.tjjs.200249.
XU G, WENG C S, KANG N, et al. Numerical simulation of gas-liquid two-phase continuous rotating detonation considering
fuel atomization [J]. Journal of Propulsion Technology, 2022, 43(1): 200249. DOI: 10.13675/j.cnki.tjjs.200249.
[35] FOX G E, DABORA E K. Breakup of liquid drops due to convective flow in shocked sprays [J]. Symposium (International)
on Combustion, 1973, 14(1): 1365–1373. DOI: 10.1016/S0082-0784(73)80122-5.
[36] KHOSLA S, CROCKER D S. CFD modeling of the atomization of plain liquid jets in cross flow for gas turbine applications [C] //
Proceedings of ASME Turbo Expo 2004: Power for Land, Sea, and Air. Vienna, Austria: American Society of Mechanical
Engineers, 2004. DOI: 10.1115/GT2004-54269.
[37] KHARE P, WANG S, YANG V. Modeling of finite-size droplets and particles in multiphase flows [J]. Chinese Journal of
Aeronautics, 2015, 28(4): 974–982. DOI: 10.1016/j.cja.2015.05.004.
[38] BROUMAND M, FAROKHI M, BIROUK M. Penetration height of a circular liquid jet in a subsonic gaseous crossflow: an
eulerian-lagrangian approach [C] // 54th AIAA Aerospace Sciences Meeting. San Diego, California, USA: AIAA, 2016. DOI:
10.2514/6.2016-1591.
[39] BHANDARKAR A, MANNA P, CHAKRABORTY D. Assessment of droplet breakup models in high-speed cross-flow [J].
Atomization and Sprays, 2017, 27(1): 61–79. DOI: 10.1615/atomizspr.2016015409.
[40] HU R, LI Q, LI C, LI C. Effects of an accompanied gas jet on transverse liquid injection in a supersonic crossflow [J]. Acta
Astronautica, 2019, 159: 440–451. DOI: 10.1016/j.actaastro.2019.01.040.
[41] BURCAT A, EIDELMAN A. Evolution of a detonation wave in a cloud of fuel droplets: part Ⅱ. influence of fuel droplets [J].
AIAA Journal, 1980, 18(10): 80–4099. DOI: 10.2514/3.7717.
[42] 吴望一. 流体力学 [M]. 北京: 北京大学出版社, 2001.
[43] LIU A B, MATHER D, REITZ R D. Modeling the effects of drop drag and breakup on fuel sprays: 930072 [R]. SAE
Transactions, Detroit, USA, 1993.
[44] O’ROURKE P J, AMSDEN A A. The TAB method for numerical calculation of spray droplet breakup [R]. Los Alamos, NM,
USA: Los Alamos National Laboratory, 1987.
[45] STEPHEN R T, DANIEL C H. An introduction to combustion: concepts and applications [M]. New York, USA: McGraw
Hill, 2000.
[46] GUO K K, NIE W S, CAI H H. Numerical simulation of damping capacity between injector-formed baffle and normal blade
baffle in a kero/lox liquid rocket engine [C] // Proceedings of the Advances in Materials, Machinery, Electical Engineering
(AMMEE 2017). Prais, France: Atlantis Press, 2017: 576–585. DOI: 10.2991/ammee-17.2017.110.
[47] KUO K K Y. Principles of combustion [M]. New York, USA: John Wiley and Sons, 1986.
(责任编辑 蔡国艳)

022101-15