1. Shen, Dawen,Cheng, Miao,Rong,
Guangyao, et al.Effects of film cooling injection inclination angle on cooling
performance in rotating detonation combustors[J].PHYSICS OF
FLUIDS,2024,36(02).DOI:10.1063/5.0188972.
2. Cheng, Miao,Sheng,
Zhaohua,Wang, JianPing.BYCFoam: An Improved Solver for Rotating Detonation
Engines Based on OpenFOAM[J].ENERGIES,2024,17(04).DOI:10.3390/en17040769.
3. Wang, Yingnan,Zhang,
Xiangjun,Liu, Peilin, et al.Effect of the inlet spatial fluctuation on the
gas-solid continuous rotating detonation flow field characteristics[J].PHYSICS
OF FLUIDS,2024,36(07).DOI:10.1063/5.0215308.
4. Zhang, Yunzhen,Cheng, Miao,Liu,
Xiangyang, et al.The influence of plug nozzle and Laval nozzle on the flow
field and performance of non-premixed rotating detonation combustor[J].PHYSICS
OF FLUIDS,2024,36(05).DOI:10.1063/5.0207508.
5. He, XiaoJian,Gong,
XiaoPeng,Wang, JianPing, et al.Investigation of the total pressure gain in
rotating detonation combustors with dilution holes[J].PHYSICS OF
FLUIDS,2024,36(04).DOI:10.1063/5.0195613.
6. He, XiaoJian,Wang, JianPing,Ma,
John Z..Investigation of the evolution process and propulsion performance of
the longitudinal pulsed detonation in rotating detonation combustors[J].PHYSICS
OF FLUIDS,2024,36(03).DOI:10.1063/5.0187773.
7. Rong, Guangyao,Cheng,
Miao,Sheng, Zhaohua, et al.Flow field characteristics and particle path
tracking of a hollow rotating detonation engine with a Laval nozzle[J].PHYSICS
OF FLUIDS,2023,35(05).DOI:10.1063/5.0144651.
8. Rong, Guangyao,Cheng,
Miao,Zhang, Yunzhen, et al.Investigation of flow field characteristics and
performance of carbon-hydrogen/oxygen-rich air rotating detonation
engine[J].PHYSICS OF FLUIDS,2023,35(09).DOI:10.1063/5.0154599.
9. Sheng, Zhaohua,Cheng,
Miao,Wang, JianPing.Multi-wave effects on stability and performance in rotating
detonation combustors[J].PHYSICS OF FLUIDS,2023,35(07).DOI:10.1063/5.0144199.
10. Shen, Dawen,Sheng,
Zhaohua,Zhang, Yunzhen, et al.Predicting combustion behavior in rotating
detonation engines using an interpretable deep learning method[J].PHYSICS OF
FLUIDS,2023,35(07).DOI:10.1063/5.0155991.
11. Wu, Wenbin,Wang, Yingnan,Wu,
Kewen, et al.Experimental evaluation of aluminum powder fuel in a
hydrogen/oxygen detonation tube[J].INTERNATIONAL JOURNAL OF HYDROGEN
ENERGY,2023,48(62):24089-24100.DOI:10.1016/j.ijhydene.2023.03.078.
12. He, XiaoJian,Liu,
XiangYang,Wang, JianPing.Numerical study of the mechanisms of the longitudinal
pulsed detonation in two-dimensional rotating detonation combustors[J].PHYSICS
OF FLUIDS,2023,35(03).DOI:10.1063/5.0136290.
13. Rong, Guangyao,Cheng,
Miao,Sheng, Zhaohua, et al.Investigation of counter-rotating shock wave and
wave direction control of hollow rotating detonation engine with Laval
nozzle[J].PHYSICS OF FLUIDS,2022,34(05).DOI:10.1063/5.0089207.
14. Rong, Guangyao,Cheng,
Miao,Sheng, Zhaohua, et al.Investigation of counter-rotating shock wave
phenomenon and instability mechanisms of rotating detonation engine with hollow
combustor and Laval nozzle[J].INTERNATIONAL JOURNAL OF HYDROGEN
ENERGY,2022,47(54):23019-23037.DOI:10.1016/j.ijhydene.2022.05.082.
15. Zhu, Wenchao,Wang, Yuhui,Wang,
Jianping.Flow field of a rotating detonation engine fueled by carbon[J].PHYSICS
OF FLUIDS,2022,34(07).DOI:10.1063/5.0099787.
16. Sheng, Zhaohua,Cheng,
Miao,Shen, Dawen, et al.An active direction control method in rotating
detonation combustor[J].INTERNATIONAL JOURNAL OF HYDROGEN
ENERGY,2022,47(55):23427-23443.DOI:10.1016/j.ijhydene.2022.05.135.