英文期刊（部分）：

1. Ye-Tao Shao, Meng Liu, and Jian-Ping Wang. Numerical investigation of Rotating Detonation Engine Propulsive Performance. Combustion Science and Technology, 182, 2010, 1586-1597 (SCI).
2. Shao Yetao, Liu Meng, Wang Jianping. Continuous Detonation Engine and Effects of Different Types of Nozzles on Its Propulsion Performance. Chinese Journal of Aeronautics, 23(6), 2010, 647-652 (SCI).2010 Continuous Detonation Engine and Effects of Different Types of Nozzle on Its Propulsion Performance.pdf
3. Shao Ye-Tao, Wang Jian-Ping. Change in Continuous detonation wave propagation mode from rotating detonation to standing detonation. Chinese Physics Letters, 27(3), 2010, 34705 (SCI).2010-Chinese Physics Letter（at）Change in Continuous Detonation Wave Propagation Mode from Rotating Detonation to Standing Detonation.pdf 
4. Shao-wu Li, Shu Wang, Jian-ping Wang, Jian-chun Mi. Effect of Turbulence Intensity on Airfoil Flow: Numerical Simulation and Experimental Measurements. Applied Mathematics and Mechanics, 32(8), 2011, 1029-1038 (SCI).Effect of Turbulence Intensity on Airfoil Flow.pdf
5. Zhou Rui, Wang Jian-ping. Numerical Investigation of Flow Particle Paths and Thermodynamic Performance of Continuously Rotating Detonation Engines. Combustion and Flame (SCI).Numerical Investigation of Flow Particle Paths and Thermodynamic Performance of Continuously Rotating Detonation Engines.pdf

6. Wu Dan, Liu Yan, Liu Yusi, and Wang Jianping. Numerical Investigation on the restabilization of hydrogen-air rotating detonation engine. International Journal of Hydrogen Energy(SCI).2014.

7. Wu Dan, Zhou Rui, Liu Meng, and Wang Jianping. Numerical investigation on the stability of rotating detonation engine. Combustion Science and Technology(SCI).2014.

8. Zhou Rui, Wu Dan, and Wang Jianping. Partical path tracking method in 2D and 3D rotating detonation engines. Chinese Physics B(SCI).2014.

9. Liu Yan, Wu Dan, Yao Songbai, and Wang Jianping. Analytical and numerical investigations of the wedge induced oblique detonation waves at low inflow Mach number. Combustion Science and Technology(SCI).2015.

10. Xin-Meng Tang, Jian-Ping Wang, Ye-Tao Shao. Three-dimensional numerical investigations of the rotating detonation engine with a hollow combustor.Combustion and Flame(SCI). 2015
11.  

12.Liu Yusi, Wang Yuhui, Li Yongsheng, Li Yang, and Wang Jianping. Spectral analysis and self-adjusting mechanism for oscillation phenomenon in hydrogen-oxygen continuously rotating detonation engine. Chinese Journal of Aeronautics(SCI).2015.

13.Songbai Yao, Meng Liu, and Jianping Wang. Numerical study of spontaneous formation of multiple detonation wave fronts in rotating detonation engine. Combustion Science and Technology(SCI).2015

中文期刊（部分）：

1. 邵业涛，刘勐，王健平。圆柱坐标系下连续旋转爆轰发动机的数值模拟。推进技术，第30卷，第6期，2009, 717-721 (EI).2009-推进技术（at）圆柱坐标系下连续旋转爆轰发动机的数值模拟.pdf
2. 邵业涛，王健平，唐新猛，石天一．连续旋转爆轰发动机流畅三维数值模拟，航空动力学报，第25卷，第8期，2010, 1717-1722 (EI).2010-航空动力学报（at）连续旋转爆轰发动机流场三维数值模拟.pdf
3. 李韶武，王庶，王健平，米建春。湍流度对翼型绕流影响的数值模拟及与实验的对比。应用数学和力学，32（8），2011, 964-972 (EI).湍流度对翼型绕流影响的数值模拟及与实验的对比.pdf
4. 周蕊，王健平。连续爆轰发动机热力学性质的数值模拟，航空动力学报，第27卷，第1期，2012, 16-24 (EI).连续爆轰发动机热力学性质的数值模拟.pdf