.39）Min Chen, Hai Long Tang, Zhi Li Zhu. "Turbofan Engine Transient Performance Simulation Based on Cooling Effectiveness" Chinese Society of Aeronautics and Astronautics Propulsion Aero-thermodynamic Subject Exchange Communication Forum, Taiyuan, 2005. (in Chinese)
.38）Min Chen, Jin Zhang, Hai Long Tang, Zhi Li Zhu, Da Ming Zhu. "Assessment on the hypersonic combined cycle augmented engine concepts with the tandem layout." Aeronautics & Astronautics Propulsion & Power Engineering Branch Forum, 2006..(in Chinese )
.37）Hui Ou Yang, Zhi Li Zhu, Min Chen. "Size and Weight Estimation of Turbine Based Combined Cycle Turbofan Engine." Chinese Society of Aeronautics and Astronautics Propulsion Aero-thermodynamic Subject Exchange Communication Forum, JiLin,2007. (in Chinese )
.36）Min Chen, Hai Long Tang, Jin Zhang. "Real-Time Performance Simulation of a Mixed-Flow Two-Spool Augmented Turbofan Engine." Journal of Aerospace Power, 2005, 20.1:13-17. (in Chinese ) （EI）
.35）Da Ming Zhu, Min Chen, Hai Long Tang, Jin Zhang. ""Over-under" concept hypersonic turbo-ramjet combined propulsion system." Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(3):263-266. (in Chinese ) （EI）
.34）Min Chen, Zhi Li Zhu, Da Ming Zhu, Hai Long Tang. "Performance Analysis Tool for Turbine Based Combined Cycle Engine Concept." Journal of Astronautics, 2006, 27(5):854-859. (in Chinese ) （EI）
.33）Min Chen, Hai Long Tang, Da Ming Zhu, Zhi Li Zhu. "Hypersonic combined cycle engine concept with tandem layout." Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(3):265-268. (in Chinese ) （EI）
.32）Bo Wang, Hai Long Tang, Ru Hao Zhong, Min Chen. "Visualize framework for aero-engine performance simulation." Journal of Aerospace Power, 2009, 24(3). ( in Chinese ) （EI）
.31）Min Chen, Hai Long Tang, Da Xiang Liu, Jie Jin. "Conceptual design of Mach number 3.5 air-breathing propulsion system." Journal of Aerospace Power, 2009, 24(7). (in Chinese ) （EI）
.30）Bin Li, Min Chen*, Zhi Li Zhu, Kun Zhang. "Steady Performance Investigation on Various Modes of an Adaptive Cycle Aero-Engine." Journal of Propulsion Technology, 2013, 34(8):1009-1015. (in Chinese ) （EI）