Numerical Investigation on Unsteady Flow of Nozzle in Rotating Detonation Engine
1.School of Aerospace Engineering,Xiamen University,Xiamen 361102,China;2.State Key Laboratory of Laser Propulsion and Application,Beijing Power Machinery Institute,Beijing 100074,China
XIA Han-qing1, HUANG Yue1, ZHANG Yi-ning2, YOU Yan-cheng1, LI Dong2, LUAN Zhen-ye1. Numerical Investigation on Unsteady Flow of Nozzle in Rotating Detonation Engine[J]. Journal of Propulsion Technology, 2021, 42(6): 1213-1222.
[1] 马 虎, 武晓松, 王 栋, 等. 旋转爆震发动机数值研究[J]. 推进技术, 2012, 33(5).
[2] 刘世杰, 林志勇, 孙明波, 等. 旋转爆震波发动机二维数值模拟[J]. 推进技术, 2010, 31(5): 634-640.
[3] Voitsekhovskii B V. Maintained Detonations[J]. Soviet Physics Doklady, 1959, 9(6):1254-1256 .
[4] Cullen R E, Nicholls J A, Ragland K W. Feasibility Studies of a Rotating Detonation Wave Rocket Motor[J]. Journal of Spacecraft and Rockets, 1966, 3(6): 893-898.
[5] Lu F K, Braun E M. Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts[J]. Journal of Propulsion and Power, 2011, 30(5): 1-18.
[6] Driscoll R, Aghasi P, George A S, et al. Three-Dimensional Numerical Investigation of Reactant Injection Variation in a H2/Air Rotating Detonation Engine[J]. International Journal of Hydrogen Energy, 2016, 41(9):5162-5175.
[7] Driscoll R, George A S, Gutmark E J. Numerical Investigation of Injection Within Axisymmetric Rotating Detonation Engine[J]. International Journal of Hydrogen Energy, 2016, 41(3): 2052-2063.
[8] Sousa J, Paniagua G, Morata E C. Thermodynamic Analysis of a Gas Turbine Engine with a Rotating Detonation Combustor[J]. Applied Energy, 2017, 195: 247-256.
[9] Yao S, Tang X, Luan M, et al. Numerical Study of Hollow Rotating Detonation Engine with Different Fuel Injection Area Ratios[J]. Proceedings of the Combustion Institute, 2017, 36(2): 2649-2655.
[10] Xu X Y. Numerical Simulation of Injection Schemes with Separate Supply of Fuel and Oxidizer Effects on Rotating Detonation Engine[J]. Acta Aeronautica ET Astronautica Sinica, 2016, 37(4): 1184-1195.
[11] Braun J, Garcia J S, Paniagua G. Evaluation of the Unsteadiness Across Nozzles Downstream of Rotating Detonation Combustors[R]. AIAA 2017-1063.
[12] Fujii J, Kumazawa Y, Matsuo A, et al. Numerical Investigation on Detonation Velocity in Rotating Detonation Engine Chamber[J]. Proceedings of the Combustion Institute, 2016, 155(6):1540-7489.
[13] 郑榆山, 王 超, 王宇辉, 等. 旋转爆震三维非预混混合特性及流场结构研究[J]. 推进技术, 2019, 40(2): 407-415.
[14] 高 剑, 马 虎, 裴晨曦, 等. 喷管对旋转爆震发动机性能影响的实验[J]. 航空动力学报, 2016, 31(10): 2443-2453.
[15] Yi T H, Lou J, Turangan C, et al. Effect of Nozzle Shapes on the Performance of Continuously-Rotating Detonation Engine[R]. AIAA 2010-152.
[16] Rankin B A, Hoke J, Schauer F. Periodic Exhaust Flow Through a Converging-Diverging Nozzle Downstream of a Rotating Detonation Engine[R]. AIAA 2014-1015.
[17] Eto S, Tsuboi N, Takayuki K, et al. Three-Dimensional Numerical Simulation of a Rotating Detonation Engine: Effects of the Throat of a Converging-Diverging Nozzle on Engine Performance[J]. Combustion Science and Technology, 2016, 188(11-12): 2105-2116.
[18] Braun J, Saracoglu B H, Paniagua G. Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles[J]. Journal of Propulsion and Power, 2016, 36(2): 2665-2672.
[19] Jourdaine N , Tsuboi N , Ozawa K , et al. Three-Dimensional Numerical Thrust Performance Analysis of Hydrogen Fuel Mixture Rotating Detonation Engine with Aerospike Nozzle[J]. Proceedings of the Combustion Institute, 2019, 37(3): 3443-3451.
[20] Kindracki J, Wolański P, Gut Z. Experimental Research on the Rotating Detonation in Gaseous Fuels-Oxygen Mixtures [J]. Shock Waves, 2011, 21(2): 75-84.
[21] Fotia M L, Schauer F, Kaemming T, et al. Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle[J]. Journal of Propulsion and Power, 2015, 32(3): 674-681.
[22] Kato Y, Ishihara K, Matsuoka K, et al. Study of Combustion Chamber Characteristic Length in Rotating Detonation Engine with Convergent-Divergent Nozzle[R]. AIAA 2016-1406.
[23] Hishida M, Fujiwara T, Wolanski P. Fundamentals of Rotating Detonations[J]. Shock Waves, 2009, 19(1).
[24] Jiang P, Liao Z, Huang Z, et al. Influence of Shock Waves on Supersonic Transpiration Cooling[J]. International Journal of Heat and Mass Transfer, 2019, 129:965-974.