@article {Zhang_2020,
	title = {Theoretical and Numerical Investigation on Total Pressure Gain in Rotating Detonation Engine},
	journal = {AIAA Journal},
	volume = {58},
	number = {11},
	year = {2020},
	month = {nov},
	pages = {4866{\textendash}4877},
	publisher = {American Institute of Aeronautics and Astronautics (AIAA)},
	doi = {10.2514/1.j059259},
	url = {https://doi.org/10.2514\%2F1.j059259},
	author = {Shu-jie Zhang and Ma, John Z. and Jianping Wang}
}
