Citation: | WANG C,ZHENG Y S,CAI J H,et al. Direct connected experimental research on hydrocarbon-fueled rotating detonation[J]. Journal of Experiments in Fluid Mechanics, 2022,36(4):1-9. doi: 10.11729/syltlx20210086 |
[1] |
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
|
[2] |
WOLAŃSKI P. Detonative propulsion[J]. Proceedings of the Combustion Institute,2013,34:125-158. doi: 10.1016/j.proci.2012.10.005
|
[3] |
LU F K,BRAUN E M. Rotating detonation wave propul-sion: experimental challenges, modeling, and engine concepts[J]. Journal of Propulsion and Power,2014,30(5):1125-1142. doi: 10.2514/1.B34802
|
[4] |
BRAUN E M,LU F K,WILSON D R,et al. Airbreathing rotating detonation wave engine cycle analysis[J]. Aerospace Science and Technology,2013,27(1):201-208. doi: 10.1016/j.ast.2012.08.010
|
[5] |
刘世杰, 王超, 蒋露欣, 等. 连续旋转爆震冲压发动机直连式试验[C]//第十六届全国激波与激波管学术会议论文. 2014.
|
[6] |
WANG C,LIU W D,LIU S J,et al. Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen[J]. International Journal of Hydrogen Energy,2015,40(30):9530-9538. doi: 10.1016/j.ijhydene.2015.05.060
|
[7] |
WANG C,LIU W D,LIU S J,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
|
[8] |
LIU S J, LIU W D, WANG Y, et al. Free jet test of continuous rotating detonation ramjet engine[C]//Proc of the 21st AIAA International Space Planes and Hypersonics Technologies Conference. 2017: 2282. doi: 10.2514/6.2017-2282
|
[9] |
阎宝林, 张义宁, 宫继双, 等. 液态碳氢燃料连续旋转爆震燃烧实验研究[C]//第五届爆震与新型推进学术会议论文. 2017.
|
[10] |
郑权,翁春生,白桥栋. 当量比对液体燃料旋转爆轰发动机爆轰影响实验研究[J]. 推进技术,2015,36(6):947-952.
ZHENG Q,WENG C S,BAI Q D. Experimental study on effects of equivalence ratio on detonation characteristics of liquid-fueled rotating detonation engine[J]. Journal of Propulsion Technology,2015,36(6):947-952.
|
[11] |
郑权,李宝星,翁春生,等. 燃烧室长度对液态燃料旋转爆轰发动机性能影响实验研究[J]. 推进技术,2018,39(12):2764-2771.
ZHENG Q,LI B X,WENG C S,et al. Experimental investigation for effects of combustor length on liquid-fueled rotating detonation engine performance[J]. Journal of Propulsion Technology,2018,39(12):2764-2771.
|
[12] |
PENG H Y,LIU W D,LIU S J,et al. The effect of cavity on ethylene-air Continuous Rotating Detonation in the annular combustor[J]. International Journal of Hydrogen Energy,2019,44(26):14032-14043. doi: 10.1016/j.ijhydene.2019.04.017
|
[13] |
ZHOU S B,MA H,CHEN S H,et al. Experimental investigation on propagation characteristics of rotating detonation wave with a hydrogen-ethylene-acetylene fuel[J]. Acta Astronautica,2019,157:310-320. doi: 10.1016/j.actaastro.2019.01.009
|
[14] |
ZHONG Y P,WU Y,JIN D,et al. Investigation of rotating detonation fueled by the pre-combustion cracked kerosene[J]. Aerospace Science and Technology,2019,95:105480. doi: 10.1016/j.ast.2019.105480
|
[15] |
胡洪波,严宇,张锋,等. 煤油富燃燃气旋转爆震燃烧实验研究[J]. 推进技术,2020,41(4):881-888.
HU H B,YAN Y,ZHANG F,et al. Experimental investigation on rotational detonation combustion with fuel-rich gases of kerosene[J]. Journal of Propulsion Technology,2020,41(4):881-888.
|
[16] |
WALTERS I V, JOURNELL C, LEMCHERFI A I, et al. Performance characterization of a natural gas-air rotating detonation engine[C]//Proc of the AIAA Propulsion and Energy 2019 Forum. 2019: 4214. doi: 10.2514/6.2019-4214
|
[17] |
BARATTA A, STOUT J B. Demonstrated low pressure loss inlet and low equivalence ratio operation of a rotating detonation engine(RDE) for power generation[C]//Proc of the AIAA Science and Technology Forum(SciTech 2020). 2020. doi: 10.2172/1817673
|
[18] |
PRAKASH S, RAMAN V, LIETZ C, et al. High fidelity simulations of a methane-oxygen rotating detonation rocket engine[C]//Proc of the AIAA Scitech 2020 Forum. 2020: 0689. doi: 10.2514/6.2020-0689
|
[19] |
LIU S J,PENG H Y,LIU W D,et al. Effects of cavity depth on the ethylene-air Continuous Rotating Detonation[J]. Acta Astronautica,2020,166:1-10. doi: 10.1016/j.actaastro.2019.09.038
|
[20] |
PENG H Y,LIU W D,LIU S J,et al. Realization of methane-air continuous rotating detonation wave[J]. Acta Astronautica,2019,164:1-8. doi: 10.1016/j.actaastro.2019.07.001
|
[21] |
王宇辉,王超,郑榆山,等. 基于乙烯或氢气的吸气式旋转爆轰发动机实验[J]. 气体物理,2018,3(6):16-25.
WANG Y H,WANG C,ZHENG Y S,et al. Experimental on air-breathing rotating detonation engine using ethylene or hydrogen[J]. Physics of Gases,2018,3(6):16-25.
|