[1] |
Wolański P. Detonative propulsion[J]. Proceedings of the Combustion Institute, 2013, 34(1):125-158. http://d.old.wanfangdata.com.cn/Periodical/yhxb201801013
|
[2] |
Anand V, George A S, Driscoll R, et al. Investigation of rotating detonation combustor operation with H2-air mixtures[J]. International Journal of Hydrogen Energy, 2016, 41(2):1281-1292. doi: 10.1016/j.ijhydene.2015.11.041
|
[3] |
Russo R M, King P I, Schauer F R, et al. Characterization of pressure rise across a continuous detonation engine[R]. AIAA-2011-6046, 2011.
|
[4] |
Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous spin detonations[J]. Journal of Propulsion and Power, 2006, 22(6):1204-1216. doi: 10.2514/1.17656
|
[5] |
Liu S, Liu W, Lin Z, et al. Experimental research on the propagation characteristics of continuous rotating detonation wave near the operating boundary[J]. Combustion Science and Technology, 2015, 187(11):1790-1804. doi: 10.1080/00102202.2015.1019620
|
[6] |
George A S, Driscoll R, Anand V, et al. On the existence and multiplicity of rotating detonations[J]. Proceedings of the Combustion Institute, 2016, 36(2):2691-2698. https://www.sciencedirect.com/science/article/pii/S1540748916301900
|
[7] |
Lin W, Zhou J, Liu S, et al. Experimental study on propagation mode of H2/air continuously rotating detonation wave[J]. International Journal of Hydrogen Energy, 2015, 40(4):1980-1993. doi: 10.1016/j.ijhydene.2014.11.119
|
[8] |
Rankin B A, Richardson D R, Caswell A W, et al. Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine[J]. Combustion and Flame, 2017, 176:12-22. doi: 10.1016/j.combustflame.2016.09.020
|
[9] |
Frolov S M, Aksenov V S, Ivanov V S, et al. Large-scale hydrogen-air continuous detonation combustor[J]. International Journal of Hydrogen Energy, 2015, 40(3):1616-1623. doi: 10.1016/j.ijhydene.2014.11.112
|
[10] |
Roy A, Ferguson D H, Sidwell T, et al. Experimental study of rotating detonation combustor performance under preheat and back pressure operation[R]. AIAA-2017-1065, 2017.
|
[11] |
Anand V, George A S, Driscoll R, et al. Longitudinal pulsed detonation instability in a rotating detonation combustor[J]. Experimental Thermal and Fluid Science, 2016, 77:212-225. doi: 10.1016/j.expthermflusci.2016.04.025
|
[12] |
Zhou R, Wang J P. Numerical investigation of flow particle paths and thermodynamic performance of continuously rotating detonation engines[J]. Combustion and Flame, 2012, 159(12):3632-3645. doi: 10.1016/j.combustflame.2012.07.007
|
[13] |
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, 31(6):674-681. https://www.researchgate.net/publication/304047379_Experimental_Study_of_the_Performance_of_a_Rotating_Detonation_Engine_with_Nozzle
|
[14] |
林伟, 周进, 林志勇, 等. H2/Air连续旋转爆震发动机推力测试(Ⅰ)单波模态下的推力[J].推进技术, 2015, 36(4):495-503.Lin W, Zhou J, Lin Z Y, et al. Thrust measurement of H2/Air continuously rotating detonation engine(Ⅰ) thrust under single wave mode[J]. Journal of Propulsion Technology, 2015, 36(4):495-503.
|
[15] |
林伟, 周进, 林志勇, 等. H2/Air连续旋转爆震发动机推力测试(Ⅱ)-双波模态下的推力[J].推进技术, 2015, 36(5):641-649. http://www.cnki.com.cn/Article/CJFDTotal-TJJS201505001.htmLin W, Zhou J, Lin Z Y, et al. Thrust measurement of H2/Air continuously rotating detonation engine(Ⅱ) thrust under dual wave mode[J]. Journal of Propulsion Technology, 2015, 36(5):641-649. http://www.cnki.com.cn/Article/CJFDTotal-TJJS201505001.htm
|
[16] |
DeBarmore N D, King P I, Schauer F R, et al. Nozzle guide vane integration into rotating detonation engine[R]. AIAA-2013-1030, 2013.
|
[17] |
Higashi J, Nakagami S, Matsuoka K, et al. Experimental study of the disk-shaped rotating detonation turbine engine[R]. AIAA-2017-1286, 2017.
|
[18] |
Bykovskii F A, Vedernikov E F. Continuous detonation of a subsonic flow of a propellant[J]. Combustion, Explosion and Shock Waves, 2003, 39(3):323-334. doi: 10.1023/A:1023800521344
|
[19] |
Wang C, Liu W, Liu S, et al. Experimental investigation on detonation combustion patterns of hydrogen/vitiated air within annular combustor[J]. Experimental Thermal and Fluid Science, 2015, 66:269-278. doi: 10.1016/j.expthermflusci.2015.02.024
|
[20] |
Yang C, Wu X, Ma H, et al. Experimental research on initiation characteristics of a rotating detonation engine[J]. Experimental Thermal and Fluid Science, 2016, 71:154-163. doi: 10.1016/j.expthermflusci.2015.10.019
|
[21] |
Lieuwen T C. Unsteady combustor physics[M]. Cambridge:Cambridge University Press, 2012.
|