Page 17 - 《爆炸与冲击》2023年第2期
P. 17

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

               [11]  FOTIA M L, KAEMMING T A, HOKE J, et al. Study of the experimental performance of a rotating detonation engine with
                    nozzled  exhaust  flow  [C]  //  53rd  AIAA  Aerospace  Sciences  Meeting.  Kissimmee,  Florida,  USA:  AIAA,  2015.  DOI:
                    10.2514/6.2015-0631.
               [12]  ISHIHARA K, KATO Y, MATSUOKA K, et al. Performance evaluation of a rotating detonation engine with conical-shape
                    tail [C] // 53rd AIAA Aerospace Sciences Meeting. Kissimmee, Florida, USA: AIAA, 2015. DOI: 10.2514/6.2015-0630.
               [13]  FOTIA M, SCHAUER F, HOKE J. Experimental study of performance scaling in rotating detonation engines operated on
                    hydrogen  and  gaseous  hydrocarbon  fuel  [C]  //  20th  AIAA  International  Space  Planes  and  Hypersonic  Systems  and
                    Technologies Conference. Glasgow, Scotland: AIAA, 2015. DOI: 10.2514/6.2015-3626.
               [14]  WANG Y H, LE J L. Rotating detonation engines with two fuel orifice schemes [J]. Acta Astronautica, 2019, 161: 262–275.
                    DOI: 10.1016/j.actaastro.2019.05.035.
               [15]  NAKAGAMI S, MATSUOKA K, KASAHARA J, et al. Visualization of rotating detonation waves in a plane combustor with
                    a  cylindrical  wall  injector  [C]  //  53rd  AIAA  Aerospace  Sciences  Meeting.  Kissimmee,  Florida,  USA:  AIAA,  2015.  DOI:
                    10.2514/6.2015-0878.
               [16]  RANKIN B A, RICHARDSON D R, CASWELL A W, et al. Imaging of OH* chemiluminescence in an optically accessible
                    nonpremixed rotating detonation engine [C] // 53rd AIAA Aerospace Sciences Meeting. Kissimmee, Florida, USA: AIAA,
                    2015. DOI: 10.2514/6.2015-1604.
               [17]  MEYER S J, POLANKA M D, SCHAUER F R, et al. Parameter impact on heat flux in a rotating detonation engine [C] // 53rd
                    AIAA Aerospace Sciences Meeting. Kissimmee, Florida, USA: AIAA, 2018. DOI: 10.2514/6.2018-0400.
               [18]  THEUERKAUF S W, SCHAUER F R, ANTHONY R, et al. Experimental characterization of high-frequency heat flux in a
                    rotating  detonation  engine  [C]  //  53rd  AIAA  Aerospace  Sciences  Meeting.  Kissimmee,  Florida,  USA:  AIAA,  2015.  DOI:
                    10.2514/6.2015-1603.
               [19]  李宝星, 许桂阳, 舒慧明, 等. 燃烧室轴向和周向长度对气液两相旋转爆轰特性的影响 [J]. 航空动力学报, 2020, 35(8):
                    1601–1611. DOI: 10.13224/j.cnki.jasp.2020.08.005.
                    LI B X, XU G Y, SHU H M, et al. Influence of axial and circumferential lengths of combustion chamber on gas-liquid two-
                    phase  rotating  detonation  characteristics  [J].  Journal  of  Aerospace  Power,  2020,  35(8): 1601–1611.  DOI:  10.13224/j.cnki.
                    jasp.2020.08.005.
               [20]  徐灿, 邓利, 马虎, 等. 环缝宽度对旋转爆震发动机工作特性的影响 [J]. 爆炸与冲击, 2019, 39(3): 032102. DOI: 10.
                    11883/bzycj-2017-0248.
                    XU C, DENG L, MA H, et al. Annular gaps width effecting on performance of rotating detonation engine [J]. Explosion and
                    Shock Waves, 2019, 39(3): 032102. DOI: 10.11883/bzycj-2017-0248.
               [21]  ZHANG L F, ZHANG S J, WANG J P. A direct simulation of continuous detonation engine with the Navier-Stokes equations [C] //
                    21st AIAA International Space Planes and Hypersonics Technologies Conference. Xiamen, Fujian, China: AIAA, 2017. DOI:
                    10.2514/6.2017-2323.
               [22]  SHAO Y T, LIU M, WANG J P. Continuous detonation engine and effects of different types of nozzle on its propulsion
                    performance [J]. Chinese Journal Aeronautics, 2010, 23(6): 647–652. DOI: 10.1016/S1000-9361(09)60266-1.
               [23]  SUN J, ZHOU J, LIU S J, et al. Numerical investigation of a non-premixed hollow rotating detonation engine [J]. International
                    Journal of Hydrogen Energy, 2019, 44(31): 17084–17094. DOI: 10.1016/j.ijhydene.2019.04.168.
               [24]  HAYASHI K A, SHIMOMURA K, TSUBOI N, et al. 3D numerical study on flow field in disc-RDE [C] // AIAA Propulsion
                    and Energy Forum. Virtual Event: AIAA, 2021. DOI: 10.25Virtual Event14/6.2021-3665.
               [25]  徐雪阳, 卓长飞, 武晓松, 等. 非预混喷注对旋转爆震发动机影响的数值研究 [J]. 航空学报, 2016, 37(4): 1184–1195. DOI:
                    10.7527/s1000-6893.2015.0195.
                    XU X Y, ZHUO C F, WU X S, et al. 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. DOI: 10.7527/
                    s1000-6893.2015.0195.
               [26]  周蕊, 李晓鹏. 连续旋转爆轰发动机冷流场的混合特性研究 [J]. 航空学报, 2016, 37(12): 3668–3674. DOI: 10.7527/s1000-
                    6893.2016.0108.
                    ZHOU R, LI X P. Numerical investigation of mixing characteristic of cold continuously rotating detonation engine [J]. Acta
                    Aeronautica et Astronautica Sinica, 2016, 37(12): 3668–3674. DOI: 10.7527/s1000-6893.2016.0108.


                                                         022101-14
   12   13   14   15   16   17   18   19   20   21   22