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[1] Hu Ma, Xiaosong Wu, Feng Feng, Dong Wang, Chenglong Yang, Changfei Zhuo. An Experimental Study on Fuel Spray-induced Vortex-Like Structures. Experimental Thermal and Fluid Science, 57, pp.335-343, 2014. SCI: 000340340300035.
[2] Hu Ma*, Zhenjuan Xia, Wei Gao, Changfei Zhuo and Dong Wang. Numerical simulation of the deflagration-to-detonation transition of iso-octane vapor in an obstacle-filled tube, International Journal of Spray and Combustion Dynamics, 2018, DOI: 10.1177/1756827718758047. SCI
[3] Hu Ma, Xiao-song Wu, Dong Wang, Wen-xiang Cai, Jie Chen, Ji-yang Diao and Pei Chen-xi. Experimental Investigation of a Reed Valve on the Performance of a Pulse Detonation Engine[J]. Int. J. Turbo Jet-Engines, 30(4), pp.375-381, 2013. SCI: 000328557300006.
[4] Hu Ma, Xiaosong Wu, Dong Wang, Jun Chen and Feng Feng. Experimental Investigation of Pulse Detonation Engine at Different Air Inlet Systems. Proc IMechE Part G: J Aerospace Engineering, 228(12), pp.2207-2214, 2014. SCI: 000342799300005.
[5] Deng, Li，Ma, Hu*，Xu, Can，Zhou, Changsheng，Liu, Xiao，Investigation on the propagation process of rotating detonation wave，Acta Astronautica，2017.10，139：278~287.
[6] Li Deng ，Hu Ma* ，Can Xu，The feasibility of mode control in rotating detonation engine，Applied Thermal Engineering，2017.10.28，2018(129)：1538~1550.
[7] Shengbing Zhou, Hu Ma*, Shuai Li, Changsheng Zhou, Daokun Liu. Experimental study of a hydrogen-air rotating detonation engine with variable air-inlet slot. International Journal of Hydrogen Energy, 2017, 43: 11253-11262.
[8] Zhou Shengbing, Ma Hu*, Li Shuai, Liu Daokun, Yan Yu, Zhou Changsheng. Effects of a turbine guide vane on hydrogen-air rotating detonation wave propagation characteristics, International Journal of Hydrogen Energy, 2017, 42(31): 20297-20305.
[9] Zhou Shengbing, Ma Hu*, Liu Daokun, Yan Yu, Li Shuai, Zhou Changsheng. Experimental study of a hydrogen-air rotating detonation combustor, International Journal of Hydrogen Energy, 2017, 42(21): 14741-14749.
[10] Shengbing Zhou, Hu Ma*, Yuan Ma, Changsheng Zhou, Daokun Liu, Shuai Li. Experimental study on a rotating detonation combustor with an axial-flow turbine. Acta Astronautica, 2018, 151: 7-14.
[11] Zhenjuan Xia, Hu Ma*, Changfei Zhuo, Changsheng Zhou. Propagation process of H2/air rotating detonation wave and influence factors in plane-radial structure, International Journal of Hydrogen Energy, 2018, 43, 4609-4622.
[12] Zhenjuan Xia , Hu Ma*, Changfei Zhuo and Changsheng Zhou. Propagation characteristics of rotating detonation wave in plane–radial structure with different pressure conditions. Proc IMechE Part G: J Aerospace Engineering, 2018, DOI: 10.1177/0954410018779300.
[13] Chenglong Yang，Xiaosong Wu，Hu Ma*，Lei Peng，Jian Gao，Experimental research on initiation characteristics of a rotating detonation engine，Experimental Thermal and Fluid Science，2016.2，71：154~163.
[14] Chenglong Yang, Hu Ma，Xiaosong Wu，A computational and experimental study of injection structure effect on H2-air rotating detonation engine，52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA Propulsion and Energy Forum, (AIAA 2016-4571)，2016.6.25-2016.6.27.
[15] Lei Peng，Dong Wang, Xiaosong Wu, Chenglong Yang，Hu Ma. Ignition experiment with automotive spark on rotating detonation engine，International Journal of Hydrogen Energy，2015.7.13，40(26)：8465~8474.
[16] 夏镇娟, 武晓松, 马虎*, 卓长飞. 圆盘结构下旋转爆震波的二维数值研究, 推进技术, 2017, 38(06): 1409-1418. EI
[17] 夏镇娟, 马虎*, 卓长飞等. 圆盘结构下旋转爆震波的不稳定传播特性. 航空学报, 2018, 39(2): 121438. EI
[18] 徐灿, 马虎*, 李健, 邓利, 余陵. 旋转爆震发动机火焰与压力波传播特性, 航空学报, 2017, 38(10): 72-80. EI
[19] 彭磊,王栋,裴晨曦, 马虎*, 杨成龙, 武晓松. 旋转爆震发动机爆震波建立过程实验研究, 推进技术, 2016.8, (10)：1801~1809. EI
[20] 高剑, 马虎*, 彭磊, 徐灿, 武晓松. 不同燃烧室长度的旋转爆震发动机实验研究, 推进技术, 2016. (10)：1991~2000. EI
[21] 高剑,马虎*,裴晨曦,徐灿,武晓松. 喷管对旋转爆震发动机性能影响的实验. 航空动力学报, 2016.10, (10)：2443~2453. EI
[22] 杨成龙, 马虎*, 彭磊, 高剑, 武晓松. H2/Air旋转爆震发动机起爆实验研究, 工程热物理学报, 2016, (05)1116~1122. EI
[23] 邓利; 马虎*, 质量流率对旋转爆震波传播速度影响实验研究, 工程热物理学报, 2017.08.20, 38(8)：1784~1789. EI
[24] 周胜兵，王栋，马虎，刘道坤，夏镇娟，李帅. 氧化剂喷注面积对旋转爆震波传播特性影响的实验研究. 推进技术，2017, 38（11）: 2634-2640. EI
[25] 徐灿, 马虎*, 严宇, 邓利, 余陵. 旋转爆震发动机工作特性试验研究, 弹道学报, 2017, 29(03): 74~81.
[26] 马 虎*，武晓松，Jan Kindracki，杨成龙，邓 利. 分开喷注方式下旋转爆震发动机三维数值模拟. 燃烧科学与技术, 2016, 22(1):9-14.
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