周长省

期刊论文

1. Luhao Wang, Tao Cai, Liang Zhu (172992), Yuze Sun, Xiong Chen, Changsheng Zhou, Weixuan Li (2026). Effect of central cone axial placement on combustion and performance in SFRJ: A numerical study under cruise conditions. Case Studies in Thermal Engineering.DOI
2. Chengyin Tu, Xiong Chen, Changsheng Zhou (2026). Exploring the ignition, combustion, and agglomeration dynamics in aluminized NEPE propellants. Combustion and Flame.DOI
3. Chengyin Tu, Xiong Chen, Changsheng Zhou (2026). Experimental and theoretical investigation of Al agglomeration process on solid propellant combustion surfaces. Case Studies in Thermal Engineering.DOI
4. Luhao Wang, Tao Cai, Xiong Chen, Changsheng Zhou, Weixuan Li (2026). Investigation on the effects of mixing plate configuration on combustion and performance characteristics of SFRJ. Acta Astronautica.DOI
5. Ming Zhu, Bin Wang, Tiantian Liu, Jiwei Yao, Xiong Chen, Changsheng Zhou, Weixuan Li (2026). An enhanced intelligent-driven learning framework for adaptive multi-objective optimization control of pintle solid-fuel rocket engines. Energy.DOI
6. Luhao Wang, Tao Cai, Xiong Chen, Changsheng Zhou, W. Li (2026). Effect of the Expansion Ratio on Combustion Oscillations in Solid-Fuel Ramjets: An Experimental and Numerical Study. Aerospace.DOI
7. Bowei Meng, Hu Ma, Chunliang Dai, Zhen-Juan Xia, Changsheng Zhou (2025). Numerical study on the integration of n-decane/air two-phase rotating detonation combustor and supersonic turbine guide vanes. Applied Thermal Engineering.DOI
8. Bowei Meng, Zhen-Juan Xia, Hu Ma, Xiao Pan, Zhuojun Ying, Chunliang Dai, Shengbing Zhou, Changsheng Zhou (2025). Numerical investigation of a two-phase non-premixed n-decane/air rotating detonation combustor with inlet-integrated slot film cooling. Applied Thermal Engineering.DOI
9. Xuan Wu, Jinsheng Xu, Jian Jun Zheng, Changsheng Zhou (2025). Time‐Stress‐Aging Superposition Principle for Predicting Long‐Term Creep Behavior of HTPB Propellants Under Accelerated Storage. Journal of Applied Polymer Science.DOI
10. Xuan Wu, Jian Zheng, Jinsheng Xu, Changsheng Zhou, Zongtao Guo (2025). Research on creep damage model and finite element simulation of HTPB propellant. Mechanics of Time-Dependent Materials.DOI
11. Ming Bo Zhu, Yingkun Li, Yingkun Li, Xiong Chen, Changsheng Zhou, Junjie Mi, Tiantian Liu, Weixuan Li (2025). Nonlinear adaptive robust control strategy of thrust regulation for pintle solid-propellant rocket motors. Energy.DOI
12. Chengyin Tu, Xiong Chen, Changsheng Zhou (2025). Effect of Al and AP Particle Size on the Thermal Decomposition, Ignition Process, and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant. Combustion Science and Technology.DOI
13. Bowei Meng, Gaoyang Ge, Guangchuan Xu, Zhenjuan Xia, Hu Ma, Shengbing Zhou, Changsheng Zhou (2025). Thermodynamic and Performance Analysis of an Integrated Combustor System for a Rotating Detonation Turbine Engine.DOI
14. Yao Li, Jinsheng Xu, Changsheng Zhou, Xiong Chen, Xiumin Yang (2025). Constitutive Model Based on Stress Relaxation for Composite Modified Double-Base Propellants and Master Curve of Relaxation Modulus. Aerospace.DOI
15. 孟博威，马虎，夏镇娟，周长省（2024）. 旋转爆轰燃烧室与涡轮导向器集成特性数值研究. 《航空学报》.
16. 吴轩，黄薇，许进升，郑健，周长省，董军超（2024）. HTPB推进剂蠕变试验及长期蠕变性能研究. 《强度与环境》.
17. Chunliang Dai, Bo Sun, Yan-Jin Man, Changsheng Zhou (2024). Effects of high-temperature and entropy layer of Mach 12 oblique shock wave. Journal of Physics, Conference Series.DOI
18. Chunliang Dai, Bo Sun, Dan Zhao, Shengbing Zhou, Changsheng Zhou, Yan-Jin Man (2024). Numerical investigations on flow and heat transfer characteristics of a high-enthalpy double-cone in thermal and chemical non-equilibrium for hypersonic propulsion. International Communications in Heat and Mass Transfer.DOI
19. Luhao Wang, Weixuan Li, Xiong Chen, Changsheng Zhou (2024). Simulation Study on the Internal Flow Field of Solid Fuel Ramjet Engine with Central Cone.DOI
20. Chengyin Tu, Xiong Chen, Fan Chen, Yuqian Zhuang, Wenxiang Cai, Yingkun Li, Weixuan Li, Changsheng Zhou, Renjie Xie (2024). Effect of aluminum and ammonium perchlorate particle sizes on the condensed combustion products characteristics of aluminized NEPE propellants. Scientific Reports.DOI
21. Jing Li, Changsheng Zhou (2024). The effect of the stress equilibrium factor on the composite case of the solid rocket motor. Journal of Physics Conference Series.DOI
22. Zhengwei Sun, Jinsheng Xu, Changsheng Zhou, Xiong Chen, Zongtao Guo, Qixuan Song (2024). Damage characteristics and failure mechanism analysis of NEPE propellant at high strain rates. Scientific Reports.DOI
23. Shizhuo Hou, Hu Ma, Gaoyang Ge, Zhenjuan Xia, Changsheng Zhou (2024). Effect of Plenum Length on Propagation Characteristics of Rotating Detonation Wave.DOI
24. 涂乘崟，凌志刚，董龙龙，庄宇倩，李映坤，周长省，蔡文祥，陈雄（2023）. NEPE推进剂燃烧表面铝团聚物动态行为研究. 《推进技术》.DOI
25. 李靖，马虎，周长省，夏镇娟（2023）. 基于ANSYS ACP的固体火箭发动机复合材料壳体强度分析. 《固体火箭技术》.
26. 孟博威，杨博，张翠珍，王奉明，马虎，夏镇娟，周长省（2023）. 面向旋转爆轰燃烧室的涡轮气动性能数值研究. 《推进技术》.
27. 涂乘崟，庄宇倩，李映坤，周长省，蔡文祥，陈雄，李唯暄（2023）. NEPE推进剂燃烧过程及铝团聚特性. 《航空动力学报》.
28. Chunliang Dai, Bo Sun, Dan Zhao, Shengbing Zhou, Changsheng Zhou, Yan-Jin Man (2023). High temperature non-equilibrium flow characteristics of impinging shock/flat-plate turbulent boundary layer interaction at Mach 8.42. The Physics of Fluids.DOI
29. Chunliang Dai, Bo Sun, Lian-Jie Yue, Shengbing Zhou, Chang-Fei Zhuo, Changsheng Zhou, Jianyi Yu (2023). Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range. Chinese Journal of Aeronautics.DOI
30. Zhen-Juan Xia, Hu Ma, Gao-Yang Ge, Yong He, Changsheng Zhou (2023). Effect of Combustor Outlet Geometry on Operating Characteristics of Disk-Shaped Rotating Detonation Engine. Aerospace.DOI
31. Tiexiang Wang, Ying-Kun Li, Min Zhu, Changsheng Zhou (2023). Influence of panel oscillation on the shock flow field in isolator under complex background wave system. Journal of Physics, Conference Series.DOI
32. Xuancheng Lu, Changsheng Zhou, Luhao Wang, Min Zhu (2023). Numerical analysis of fuel regression rate and flow field in solid fuel ramjet with the gas generator. Journal of Physics, Conference Series.DOI
33. Sainan Xue, Xin Zhang, Jianlu Yang, D. Liu, Huai-Lung Ma, Changsheng Zhou (2023). Experimental study on the rotating detonation engine based on a gas mixture. Frontiers in Energy Research.DOI
34. Wang shuang-hong, Changsheng Zhou, Han chao-fan (2023). The aging property and storage life prediction of EPDM. Journal of Physics Conference Series.DOI
35. Yao Li, Changsheng Zhou, Xiumin Yang (2023). Effect of pre-fatigue on mechanical properties of modified double-base propellant. Journal of Physics Conference Series.DOI
36. 代春良，孙波，卓长飞，马虎，周长省（2022）. 前缘钝化和化学非平衡效应对斜爆震发动机进气道特性的影响. 《推进技术》.DOI
37. 葛高杨，马虎，夏镇娟，马元，侯世卓，邓利，周长省（2022）. 环缝宽度对两相旋转爆轰波压力与频率特性影响实验研究. 《推进技术》.
38. 葛高杨，马元，夏镇娟，侯世卓，马虎，邓利，周长省（2022）. 高总温空气与汽油燃料的旋转爆震验证试验. 《推进技术》.
39. 王鹏博，郑健，许进升，周长省（2022）. 固体火箭发动机推进剂/衬层界面粘接性能的仿真研究. 《固体火箭技术》.
40. 郑健，蔡成，周长省（2022）. 钨渗铜喉衬复合结构喷管热-结构耦合分析. 《固体火箭技术》.
41. 涂乘崟，陈雄，周长省，张北辰，李连波（2022）. NEPE推进剂在氮气及空气中的点火燃烧特性. 《含能材料》.
42. 丁伍，许进升，周长省，王庭钰，侯宇菲（2022）. HTPB推进剂/衬层界面Ⅰ型破坏温度相关特性. 《含能材料》.
43. Gao-Yang Ge, L. Deng, Hu Ma, Zhen-Juan Xia, Xiao Liu, Changsheng Zhou (2022). Effect of high-pressure detonation products on fuel injection and propagation characteristics of detonation wave. Propulsion and Power Research.DOI
44. Chunliang Dai, Bo Sun, Chang-Fei Zhuo, Sheng-Bing Zhou, Changsheng Zhou, Lian-Jie Yue (2022). Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow. Aerospace Science and Technology.DOI
45. Zhen-Juan Xia, Cui-Zhen Zhang, Feng-Ming Wang, Yong He, Hu Ma, Gao-Yang Ge, Changsheng Zhou (2022). Propagation characteristics of hydrogen-air rotating detonation wave in disk-shaped combustors with different configurations. Aerospace Science and Technology.DOI
46. Cheng-Yin Tu, Yaya Feng, Z. Ling, Xiong Chen, Changsheng Zhou, Ying-Kun Li, Wei-Xuan Li, W. Cai (2022). Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa. International Journal of Aerospace Engineering.DOI
47. Sainan Xue, Zhuojun Ying, Hu Ma, Changsheng Zhou (2022). Experimental Investigation on Two-Phase Rotating Detonation Fueled by Kerosene in a Hollow Directed Combustor. Frontiers in Energy Research.DOI
48. Zhen-Juan Xia, Hu Ma, Yong He, Gao-Yang Ge, Changsheng Zhou (2022). Visual experimental research on the propagation instabilities in a plane-radial rotating detonation engine. Aerospace Science and Technology.DOI
49. Hao Zhou, Caixin Chen, Feng Feng, Changsheng Zhou, Wen-Ling Zhang, Wei-Tao Wu (2022). Study of Thixotropic Characteristics of a Kerosene Gel Propellant by Bayesian Optimization. Gels.DOI
50. Hao Zhou, F. Feng, Q. Cao, Changsheng Zhou, Wei-Tao Wu, M. Massoudi (2022). Heat Transfer and Flow of a Gel Fuel in Corrugated Channels. Energies.DOI
51. Sheng-Bing Zhou, Hu Ma, Yuan Ma, Changsheng Zhou, N. Hu (2022). Investigation on C2H4-Air combustion mode in a non-premixed rotating detonation combustor. Propulsion and Power Research.DOI
52. Sainan Xue, Hu Ma, Feng-Ming Wang, Cui-Zhen Zhang, Can Xu, Chang-Fei Zhuo, Changsheng Zhou (2022). Numerical Investigation on the Height of Detonation Wave in Rotating Detonation Engine. Journal of Physics, Conference Series.DOI
53. Cheng-Yin Tu, Xiong Chen, Ying-Kun Li, Bei-chen Zhang, Changsheng Zhou (2022). Experimental study of Al agglomeration on solid propellant burning surface and condensed combustion products. Defence Technology.DOI
54. Chunliang Dai, Bo Sun, Sheng-Bing Zhou, Chang-Fei Zhuo, Changsheng Zhou, Lian-Jie Yue (2022). Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet. Acta Astronautica.DOI
55. Shuanghong Wang, Jinsheng Xu, Hui Li, Jiaming Liu, Changsheng Zhou (2022). The effect of thermal aging on the mechanical properties of ethylene propylene diene monomer charge coating. Mechanics of Time-Dependent Materials.DOI
56. 夏镇娟，张义宁，马虎，葛高杨，周长省（2021）. 点火位置对圆盘结构下旋转爆震波起爆过程的影响. 《推进技术》.DOI
57. 杨玉龙，郑健，陈雄，周长省（2021）. 长尾喷管传热及烧蚀特性研究. 《推进技术》.DOI
58. 葛高杨，郭敬涛，靳乐，马虎，夏镇娟，邓利，周长省（2021）. 旋转爆震冲压发动机总体性能分析. 《推进技术》.DOI
59. 葛高杨，马元，侯世卓，夏镇娟，马虎，邓利，周长省（2021）. 当量比对汽油燃料两相旋转爆轰发动机工作特性影响实验研究. 《爆炸与冲击》.
60. 宋峻，李辉，王士欣，许进升，周长省（2021）. 考虑应变率和环境压强的NEPE推进剂力学性能实验研究. 《兵器装备工程学报》.
61. 孙政伟，许进升，周长省，陈雄，杜红英（2021）. NEPE推进剂低高应变率下改进的黏-超弹本构模型. 《爆炸与冲击》.
62. Sheng-Bing Zhou, Hu Ma, Yuan Ma, Changsheng Zhou, Ning Hu (2021). Experimental investigation on detonation wave propagation mode in the start-up process of rotating detonation turbine engine. Aerospace Science and Technology.DOI
63. Chunliang Dai, Bo Sun, Changsheng Zhou, Chang-Fei Zhuo, Lei Du, Sheng-Bing Zhou (2021). Numerical investigation of real-gas effect of inward-turning inlet at Mach 12.DOI
64. Yu-Fei Hou, Jin-Sheng Xu, Changsheng Zhou, Xiong Chen (2021). Microstructural simulations of debonding, nucleation, and crack propagation in an HMX-MDB propellant.DOI
65. Zhen-Juan Xia, Hu Ma, Yong He, Gao-Yang Ge, Changsheng Zhou (2021). Low frequency instability in a H2/air plane-radial rotating detonation engine. International journal of hydrogen energy.DOI
66. Yu-Fei Hou, Jin-Sheng Xu, Changsheng Zhou, Xiong Chen (2021). Microstructural simulation of initial particle-matrix interfacial defect in HTPB solid propellants. Journal of Physics, Conference Series.DOI
67. Sheng-Bing Zhou, Hu Ma, Changsheng Zhou, Ning Hu (2021). Experimental research on the propagation process of rotating detonation wave with a gaseous hydrocarbon mixture fuel. Acta Astronautica.DOI
68. 侯宇菲，许进升，古勇军，周长省（2020）. 基于内聚力法则的高能硝酸酯增塑聚醚推进剂开裂过程细观模型. 《兵工学报》.
69. 侯宇菲，许进升，周长省，陈雄，李宏文（2020）. 复合固体推进剂颗粒与基体初始界面有无缺陷的细观模型对比. 《兵工学报》.
70. 邱爽，苏莹莉，杨海涛，陈雄，周长省（2020）. 推进剂组分对固体燃料冲压发动机性能的影响. 《航空动力学报》.DOI
71. 马坤，朱亮，陈雄，李映坤，周长省（2020）. 高超声速流场支杆射流减阻降热的流热耦合. 《航空动力学报》.DOI
72. 夏镇娟，马虎，葛高杨，卓长飞，周长省（2020）. 当量比对圆盘结构下旋转爆震波传播的影响. 《气体物理》.DOI
73. 周景亮，陈雄，柴金宝，周长省（2020）. 可变流量燃气发生器压强自适应控制方法研究. 《计算机仿真》.
74. 周景亮，陈雄，柴金宝，李心怡，李旭东，周长省（2020）. 固体火箭冲压发动机流量可调燃气发生器控制算法. 《航空动力学报》.
75. Zhen-Juan Xia, Hu Ma, Gao-Yang Ge, Changsheng Zhou (2020). Effects of ignition condition on the initiation characteristics of rotating detonation wave in plane-radial structure.DOI
76. Kun Ma, Ying-Kun Li, Liang Zhu, Xiong Chen, Changsheng Zhou (2020). Spike root oblique jet effect on drag and heat load reduction performance for hypersonic vehicles.DOI
77. Zhen-Juan Xia, Hu Ma, Gao-Yang Ge, Shi-Cheng Liu, Changsheng Zhou, Yong He (2020). Visual experimental investigation on stable operating process of the plane-radial rotating detonation engine.DOI
78. Min Zhu, Xiong Chen, Changsheng Zhou, Jin-Sheng Xu, O. Musa (2020). Numerical Study of Micron-Scale Aluminum Particle Combustion in an Afterburner Using Two-Way Coupling CFD–DEM Approach.DOI
79. Lian-Bo Li, Xiong Chen, Changsheng Zhou, Wei-Xuan Li, Min Zhu (2020). Experimental and model investigation on agglomeration of aluminized fuel-rich propellant in solid fuel ramjet. Combustion and Flame.DOI
80. Zhen-Juan Xia, Hu Ma, Gao-Yang Ge, Changsheng Zhou (2020). Visual experimental investigation on initiation process of H2/air rotating detonation wave in plane-radial structure.DOI
81. Lian-Bo Li, Xiong Chen, Changsheng Zhou, Min Zhu, O. Musa (2020). Experimental and numerical investigations of the effect of pressure and oxygen concentration on combustion characteristics of Al/Mg fuel-rich propellants.DOI
82. 侯宇菲，许进升，陈雄，周长省，朱亮（2019）. 考虑颗粒形状的复合固体推进剂细观损伤分析. 《固体火箭技术》.
83. 马虎，谢宗齐，邓利，薛赛男，周长省（2019）. 旋转爆震发动机轴向脉冲爆震模态的实验研究. 《实验流体力学》.
84. 李尧，许进升，周长省，冯自瑞（2019）. HTPB推进剂温度及率效应的累积损伤模型研究. 《固体火箭技术》.
85. 李唯暄，陈雄，周长省，MUSA Omer（2019）. 旋流燃烧室对固体燃料冲压发动机药柱表面传热以及燃速的影响. 《航空动力学报》.DOI
86. Sheng-Bing Zhou, Hu Ma, Yuchen Yang, Changsheng Zhou (2019). Investigation on propagation characteristics of rotating detonation wave in a radial-flow turbine engine combustor model. Acta Astronautica.DOI
87. Zhen-Juan Xia, Hu Ma, Chuan Liu, Chang-Fei Zhuo, Changsheng Zhou (2019). Experimental investigation on the propagation mode of rotating detonation wave in plane-radial combustor. Experimental Thermal and Fluid Science.DOI
88. Zhen-Juan Xia, Hu Ma, Chang-Fei Zhuo, Changsheng Zhou (2019). Propagation characteristics of rotating detonation wave in plane–radial structure with different pressure conditions.DOI
89. Sheng-Bing Zhou, Hu Ma, Sihe Chen, Ye-Pan Zhong, Changsheng Zhou (2019). Experimental investigation on propagation characteristics of rotating detonation wave with a hydrogen-ethylene-acetylene fuel. Acta Astronautica.DOI
90. L. Deng, Hu Ma, Xiao Liu, Changsheng Zhou (2019). Secondary shock wave in rotating detonation combustor.DOI
91. Min Zhu, Xiong Chen, Changsheng Zhou, Jin-Sheng Xu (2019). Experimental and numerical study of a full-size direct-connect dual-inlet DRE with a fuel-rich metalized solid propellant. International Journal of Heat and Mass Transfer.DOI
92. Gao-Yang Ge, L. Deng, Hu Ma, Xiao Liu, Le Jin, Changsheng Zhou (2019). Effect of blockage ratio on the existence of multiple waves in rotating detonation engine. Acta Astronautica.DOI
93. 王鸿丽，许进升，刘宗魁，童心，周长省（2018）. 复合改性双基推进剂黏弹性-黏塑性-黏损伤本构模型研究. 《兵工学报》.
94. 李唯暄，陈雄，周长省，杜红英（2018）. 旋流燃烧室构型对固体燃料冲压发动机自持燃烧性能影响. 《推进技术》.
95. 朱亮，陈雄，周长省，李映坤（2018）. 侧向喷流对超声速流动中支杆减阻降热特性影响的研究. 《推进技术》.
96. 童心，陈雄，许进升，杜红英，周长省（2018）. 循环加载下复合推进剂的能量耗散. 《航空学报》.
97. 夏镇娟，马虎，卓长飞，周长省（2018）. 圆盘结构下旋转爆震波的不稳定传播特性. 《航空学报》.
98. 夏镇娟，周胜兵，马虎，卓长飞，周长省（2018）. 圆盘结构下旋转爆震波传播特性的实验研究. 《爆炸与冲击》.
99. 封涛，许进升，李昊，周长省（2018）. 考虑初始界面缺陷的复合固体推进剂力学性能研究. 《弹箭与制导学报》.
100. 邓利，马虎，武晓松，周长省（2018）. 刚性源项处理方法在爆震模拟中的应用对比. 《爆炸与冲击》.
101. 周胜兵，马虎，李帅，周长省（2018）. 旋转爆震燃烧室与涡轮导向器组合实验研究. 《气体物理》.
102. 封涛，许进升，陈雄，周长省（2018）. 复合固体推进剂颗粒/基体界面参数反演优化. 《计算机仿真》.
103. 封涛，许进升，韩龙，陈雄，周长省（2018）. 初始缺陷对复合固体推进剂力学性能影响的数值研究. 《功能材料》.
104. 封涛，许进升，韩龙，陈雄，周长省（2018）. 细观结构对HTPB推进剂力学性能影响的数值研究. 《功能材料》.
105. 封涛，许进升，范兴贵，韩龙，陈雄，周长省（2018）. 考虑初始缺陷的HTPB推进剂粘超弹本构模型. 《含能材料》.
106. 李辉，许进升，周长省，陈雄，郑健（2018）. HTPB推进剂温度相关性失效准则. 《含能材料》.
107. 封涛，许进升，韩龙，陈雄，周长省（2018）. 含初始缺陷的复合固体推进剂力学性能. 《航空材料学报》.
108. 王鸿丽，许进升，陈雄，周长省（2018）. 固体火箭推进剂过保温后力学性能试验研究. 《弹道学报》.
109. Liang Zhu, Xiong Chen, Ying-Kun Li, O. Musa, Changsheng Zhou (2018). Investigation of drag and heat reduction induced by a novel combinational lateral jet and spike concept in supersonic flows based on conjugate heat transfer approach.DOI
110. Zhen-Juan Xia, Hu Ma, Chang-Fei Zhuo, Changsheng Zhou (2018). Propagation process of H2/air rotating detonation wave and influence factors in plane-radial structure.DOI
111. Lunkun Gong, Xiong Chen, O. Musa, Yingli Su, Changsheng Zhou (2018). Combustion Characteristics of the Solid-Fuel Ramjet with Star Solid Fuel. Journal of Aerospace Engineering.DOI
112. Sheng-Bing Zhou, Hu Ma, Shuaiyi Li, Changsheng Zhou, Dao-Kun Liu (2018). Experimental study of a hydrogen-air rotating detonation engine with variable air-inlet slot. International journal of hydrogen energy.DOI
113. Sheng-Bing Zhou, Hu Ma, Yuan Ma, Changsheng Zhou, Dao-Kun Liu, Shuaiyi Li (2018). Experimental study on a rotating detonation combustor with an axial-flow turbine. Acta Astronautica.DOI
114. L. Deng, Hu Ma, Can Xu, Xiao Liu, Changsheng Zhou (2018). The feasibility of mode control in rotating detonation engine.DOI
115. Lian-Bo Li, Xiong Chen, O. Musa, Changsheng Zhou, Min Zhu (2018). The effect of pressure and oxygen concentration on the ignition and combustion of aluminum–magnesium fuel-rich propellant.DOI
116. Ying-Kun Li, Xiong Chen, Jin-Sheng Xu, Changsheng Zhou, O. Musa (2018). Three-dimensional multi-physics coupled simulation of ignition transient in a dual pulse solid rocket motor.DOI
117. Sheng-Bing Zhou, Hu Ma, Chuan Liu, Changsheng Zhou, Dao-Kun Liu (2018). Experimental investigation on the temperature and heat-transfer characteristics of rotating-detonation-combustor outer wall. International journal of hydrogen energy.DOI
118. Omer Musa, Xiong Chen, Changsheng Zhou, Li Ying-kun, Liao Wen-He (2018). Investigations on the influence of swirl intensity on solid-fuel ramjet engine. Computers & Fluids.DOI
119. 王鸿丽，许进升，陈雄，周长省（2017）. 改性双基推进剂黏弹-黏塑性本构模型. 《航空学报》.
120. 叶小兵，陈雄，单新有，周长省，秦振杨（2017）. 膏体推进剂火箭发动机点火特性. 《含能材料》.
121. 巩伦昆，陈雄，李唯暄，杨海涛，周长省（2017）. 固体燃料冲压发动机自持燃烧的影响因素. 《航空学报》.
122. 邓利，马虎，张云锋，徐灿，周长省（2017）. 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》.
123. 王鸿丽，许进升，周长省，靳青梅（2017）. 改性双基推进剂拉压不对称力学性能研究. 《固体火箭技术》.
124. 韩龙，陈雄，许进升，周长省，赵磊（2017）. 基于细观模型的复合推进剂宏观松弛行为. 《固体火箭技术》.
125. 薛海峰，陈雄，郑健，周长省（2017）. 炭/酚醛燃气舵烧蚀性能. 《固体火箭技术》.
126. 李映坤，韩珺礼，陈雄，周长省，巩伦昆（2017）. 基于多物理场耦合的双脉冲发动机点火过程数值模拟. 《航空学报》.
127. 杨晓红，许进升，周长省，李宏文，杜红英（2017）. 三元乙丙橡胶热氧老化后的力学性能. 《北京理工大学学报》.
128. 赖华锦，陈雄，周长省，相恒升（2017）. 负压环境下铝镁贫氧推进剂激光点火及燃烧特性. 《含能材料》.
129. 相恒升，陈雄，周长省，赖华锦（2017）. 环境氧含量和压力对铝镁贫氧推进剂燃烧性能的影响. 《含能材料》.
130. 韩龙，许进升，周长省（2017）. 基体特性对HTPB推进剂力学性能的影响. 《航空动力学报》.
131. 李昊，许进升，王鸿丽，周长省（2017）. 发动机装填蜂巢状药型安全力学特性研究. 《计算机仿真》.
132. Xiong Chen, Changsheng Zhou, Min Zhu, O. Musa (2017). Combustion modeling of unsteady reacting swirling flow in solid fuel ramjet. 2017 International Conference on Mechanical, System and Control Engineering (ICMSC).DOI
133. Jin-Sheng Xu, Long Han, Jian-Ye Zheng, Xiong Chen, Changsheng Zhou (2017). Finite element implementation of a thermo-damage-viscoelastic constitutive model for hydroxyl-terminated polybutadiene composite propellant. Mechanics of Time-Dependent Materials.DOI
134. Lunkun Gong, Xiong Chen, Hai-Bo Yang, Wei-Xuan Li, Changsheng Zhou (2017). Investigation on the effect of diaphragm on the combustion characteristics of solid-fuel ramjet.DOI
135. L. Deng, Hu Ma, Can Xu, Changsheng Zhou, Xiao Liu (2017). Investigation on the propagation process of rotating detonation wave.DOI
136. Xiong Chen, Changsheng Zhou, Min Zhu, O. Musa (2017). Validation of multi-physics coupling code for unsteady reacting swirling flow in solid fuel ramjet. 2017 2nd International Conference on Frontiers of Sensors Technologies (ICFST).DOI
137. Sheng-Bing Zhou, Hu Ma, Dao-Kun Liu, Yu Yan, Shuaiyi Li, Changsheng Zhou (2017). Experimental study of a hydrogen-air rotating detonation combustor.DOI
138. Lian-Bo Li, Xiong Chen, Changsheng Zhou, Min Zhu, O. Musa (2017). Experimental Investigation on Ignition Characteristic of NEPE Propellant. 30th International Symposium on Ballistics.DOI
139. Lian-Bo Li, Xiong Chen, Changsheng Zhou, Min Zhu, O. Musa (2017). Experimental Investigation on Laser Ignition and Combustion Characteristics of NEPE Propellant.DOI
140. Min Zhu, Xiong Chen, Changsheng Zhou (2017). Numerical Investigations on the Combustion Characteristics of Single Magnesium Particle in the Forced-Convective Flow.DOI
141. Sheng-Bing Zhou, Hu Ma, Shuaiyi Li, Dao-Kun Liu, Yu Yan, Changsheng Zhou (2017). Effects of a turbine guide vane on hydrogen-air rotating detonation wave propagation characteristics.DOI
142. Hai-Feng Xue, Xiong Chen, Jian Zheng, Changsheng Zhou (2017). Contrastive Research about Fluid-thermal Coupling of Carbon-phenolic Jet Vane in Terms of Two Different Numerical Models.DOI
143. Min Zhu, Xiong Chen, Changsheng Zhou, Jin-Sheng Xu, O. Musa, Heng-Sheng Xiang (2017). Experimental and numerical investigations on the decomposition and combustion characteristics of composite propellant with Mg/Al particles additives.DOI
144. Huajun Lai, Xiong Chen, Changsheng Zhou, Heng-Sheng Xiang (2017). Study on the laser irradiation characteristics of Al/Mg fuel-rich propellant at lower ambient pressures. Selected Proceedings from CSOE.DOI
145. Zhen-hua Shen, Xiong Chen, Changsheng Zhou (2017). Numerical Simulation of Solid Fuel Ramjet Combustion Chamber Under Different Air Fuel Ratio.DOI
146. Lunkun Gong, Xiong Chen, O. Musa, Hai-Bo Yang, Changsheng Zhou (2017). Numerical and experimental investigation of the effect of geometry on combustion characteristics of solid-fuel ramjet.DOI
147. 刘锐，陈雄，周长省，于溪（2016）. 基于三维激光扫描技术的喷管烧蚀形貌数据重构及分析. 《固体火箭技术》.
148. 巩伦昆，陈雄，周长省，李映坤，朱敏（2016）. 来流条件对SFRJ燃速及自持燃烧性能的影响. 《航空学报》.
149. 刘锐，陈雄，周长省，李映坤（2016）. 非正交界面下的插值耦合传热方法. 《推进技术》.
150. 巩伦昆，陈雄，周长省，李映坤，朱敏（2016）. 结构尺寸对固体燃料冲压发动机燃速影响的仿真研究. 《兵工学报》.
151. 郑健，赵超，周长省，许进升，陈雄（2016）. 改性双基推进剂断裂能下限研究. 《推进技术》.
152. 薛海峰，陈雄，周长省（2016）. 碳/酚醛燃气舵热化学烧蚀过程数值研究. 《推进技术》.
153. 郑健，余家泉，周长省，贾登（2016）. 基于内聚力模型的改性双基推进剂断裂特性研究. 《推进技术》.
154. 郑健，陈雄，周长省，许进升（2016）. 一种插入式组合喷管的设计方法与实验研究. 《固体火箭技术》.
155. 相恒升，陈雄，周长省，赖华锦（2016）. 环境气体氧含量对NEPE推进剂激光点火过程的影响. 《火炸药学报》.DOI
156. 马赛尔，许进升，童心，周长省，李昊（2016）. 高密度聚乙烯单轴拉伸力学性能及本构关系研究. 《中国塑料》.
157. 张中水，周长省，许进升，陈雄（2016）. 基于EPDM热解材料的力学性能研究. 《弹箭与制导学报》.
158. 杜镇志，陈雄，李映坤，周长省（2016）. 超音速电弧加热等离子发动机的数值研究. 《真空科学与技术学报》.
159. 郑健，汪文强，陈雄，周长省，许进升（2016）. 基于Hopkinson技术的CMDB推进剂动态起裂韧性实验. 《航空动力学报》.
160. 赖华锦，陈雄，周长省，相恒升（2016）. 低压环境下铝镁贫氧推进剂激光辐照特性研究（英文）. 《强激光材料与元器件学术研讨会暨激光破坏学术研讨会》.
161. 韩龙，许进升，周长省（2016）. HTPB/IPDI复合固体推进剂细观界面率相关参数的反演识别研究. 《含能材料》.
162. Long Han, Jin-Sheng Xu, Changsheng Zhou（2016）. HTPB/IPDI/複合複合固体推進剤の逆相関パラメータの反転認識に関する研究【JST・京大機械翻訳】.
163. Shao-Qing Hu, Jin-Sheng Xu, Long Han, Changsheng Zhou (2016). Experimental Study on the Rate Correlativity of Particulate-filled Composite.DOI
164. Jian-Ye Zheng, Jia-Quan Yu, Changsheng Zhou, Deng Jia（2016）. 結合力モデルに基づくダブル推進剤の特性はYan究である。【JST・京大機械翻訳】.
165. Heng-Sheng Xiang, Xiong Chen, Changsheng Zhou (2016). Study on the laser irradiation characteristics of NEPE propellant in different oxygen concentrations. Selected Proceedings from CSOE.DOI
166. Hai-Feng Xue, Xiong Chen, Changsheng Zhou（2016）. 炭素/フェノール系の熱化学的アブレーション過程の数値的研究【JST・京大機械翻訳】.
167. Jian-Ye Zheng, Jia-Quan Yu, Changsheng Zhou, Deng Jia (2016). Research on Fracture Property of CMDB Propellant Based on Cohesive Zone Model.
168. Heng-Sheng Xiang, Xiong Chen, Changsheng Zhou, Huajun Lai (2016). Effect of Oxygen Content in Environment Gas on the Laser Ignition Process of NEPE Propellant.
169. Qing-Chun Zhou, Jin-Sheng Xu, Xiong Chen, Changsheng Zhou (2016). Review of the Adhesively Bonded Interface in a Solid Rocket Motor.DOI
170. Jian Zheng, Chao Zhao, Changsheng Zhou, Jin-Sheng Xu, Xiong Chen（2016）. ダブル推進推進剤の下限研究【JST・京大機械翻訳】.
171. 余家泉，许进升，陈雄，周长省，贾登，李宏文（2015）. 推进剂/包覆层界面脱粘率相关特性研究. 《航空学报》.
172. 汪文强，郑健，陈雄，赵超，许进升，周长省（2015）. 基于扩展有限元的改性双基推进剂的开裂过程模拟研究. 《推进技术》.
173. 周长省（2015）. 野战火箭发动机设计.
174. 薛海峰，陈雄，周长省（2015）. 基于热解过程的变热物性碳/酚醛能量扩散数值研究. 《固体火箭技术》.
175. 郑健，汪文强，陈雄，许进升，周长省（2015）. 基于微观结构分析的CMDB推进剂动态断裂韧性加载率敏感性研究. 《推进技术》.
176. 刘锐，陈雄，周长省，李映坤（2015）. 复合结构喷管烧蚀形貌的测定及其对流场的影响. 《航空学报》.
177. 汪文强，陈雄，郑健，赵超，许进升，周长省（2015）. 冲击载荷下CMDB推进剂断裂性能实验研究. 《固体火箭技术》.
178. 汪文强，郑健，许进升，陈雄，周长省（2015）. AP/Al/CMDB推进剂的断裂特性实验研究. 《推进技术》.
179. 余家泉，郑健，周清春，周长省，贾登（2015）. CMDB/EPDM包覆界面脱粘性能研究. 《固体火箭技术》.
180. 余家泉，陈雄，周长省，高艳宾，杜红英（2015）. EPDM薄膜橡胶包覆材料的粘-超弹本构模型研究. 《推进技术》.
181. 薛海峰，陈雄，郑健，周长省（2015）. 基于热解动力学炭/酚醛燃气舵流热耦合数值研究. 《固体火箭技术》.
182. 韩龙，陈雄，赵亚楠，许进升，周长省（2015）. 基于累积损伤模型的NEPE推进剂温度及率相关破坏准则研究. 《推进技术》.
183. 杜镇志，陈雄，周长省，王轶（2015）. 基于不同湍流模型的电弧加热等离子射流数值模拟. 《真空科学与技术学报》.
184. 周俊，周长省，陈雄（2015）. 基于BP神经网络固冲发动机燃气流量调节控制. 《计算机仿真》.
185. 陈浩，陈雄，周长省，薛海峰（2015）. 超音速等离子体炬的磁流体动力学数值研究. 《高压物理学报》.
186. 周清春，鞠玉涛，周长省（2015）. 基于Hooke-Jeeves算法的挠性粘接件的高效内聚反演分析. 《工程力学》.
187. 蒋晶，周长省，赵磊，陈雄，许进升（2015）. EPDM包覆层材料静动态压缩实验研究. 《弹箭与制导学报》.
188. Qing-Chun Zhou, Xiong Chen, R. Niu, Changsheng Zhou (2015). Extraction of rate-dependent fracture properties of adhesive interface involving large-scale yielding.DOI
189. Zhen-Zhi Du, Xiong Chen, Ying-Kun Li, Changsheng Zhou (2015). Effect of Anode Structure on the Plasma Jet Characteristics of Arcjet Thruster.DOI
190. Zhen-Zhi Du, Xiong Chen, Ying-Kun Li, Changsheng Zhou (2015). Effect of node tructure on the lasma et haracteristics of rcjet hruster.
191. Qing-Chun Zhou, Jin-Sheng Xu, Xiong Chen, Jian-Ye Zheng, Changsheng Zhou (2015). Stress singularity in a rectangular bond specimen of a solid rocket motor: Effects and elimination.DOI
192. Long Han, Xiong Chen, Jin-Sheng Xu, Changsheng Zhou, Jia-Quan Yu (2015). Research on the time–temperature–damage superposition principle of NEPE propellant. Mechanics of Time-Dependent Materials.DOI
193. Jia-Quan Yu, Jian-Ye Zheng, D. Jia, Changsheng Zhou (2015). Finite Element Modeling of Propellant and Inhibitor Interface Debonding.DOI
194. Rui Liu, Xiong Chen, Changsheng Zhou, Li Ying-Kun (2015). A Couple Approach for a Conjugate Heat Transfer Investigation of the Shape-Change Effects in a Composite Nozzle. Numerical Heat Transfer Part A Applications.DOI
195. 成红刚，陈雄，朱国强，周长省，鞠玉涛（2014）. PE在固体燃料冲压发动机中的燃烧特性实验研究. 《固体火箭技术》.
196. 郑健，张建彬，周长省，王文平（2014）. 蠕变试验下固体推进剂泊松比研究. 《南京理工大学学报》.
197. 陈雄，成红刚，周长省，朱国强（2014）. 聚乙烯在固体燃料冲压发动机中的燃速影响因素研究. 《兵工学报》.
198. 杨晓红，许进升，孙俊丽，胡少青，周长省（2014）. 三元乙丙材料粘超弹本构模型研究. 《兵工学报》.
199. 周清春，鞠玉涛，韦震，周长省（2014）. 端羟基聚丁二烯推进剂/衬层脱粘的断裂机理与断裂能获取研究. 《兵工学报》.
200. 钮然铭，陈雄，周长省，周清春（2014）. 基于损伤的HTPB推进剂/衬层界面内聚法则构建. 《固体火箭技术》.
201. 刘锐，陈雄，周长省，李映坤（2014）. 不同膨胀状态下拉瓦尔喷管内耦合传热数值研究. 《固体火箭技术》.
202. 胡少青，鞠玉涛，韦震，周长省（2014）. HTPB/IPDI弹性体的粘-超弹性本构模型研究. 《固体火箭技术》.
203. 胡少青，鞠玉涛，韦震，周长省（2014）. 双基推进剂的切口强度及切口敏感性. 《航空动力学报》.
204. Jin-Sheng Xu, Chen Xiong, Hong-Li Wang, Jian-Ye Zheng, Changsheng Zhou (2014). Thermo-damage-viscoelastic constitutive model of HTPB composite propellant.DOI
205. Qing-Chun Zhou, Yu Ju, Zhen Wei, Bo Han, Changsheng Zhou (2014). Cohesive Zone Modeling of Propellant and Insulation Interface Debonding.DOI
206. 张建彬，鞠玉涛，周长省（2013）. 双基固体推进剂的特性研究. 《固体火箭技术》.
207. 韩波，鞠玉涛，周长省（2013）. HTPB推进剂粘聚断裂研究. 《固体火箭技术》.
208. 胡少青，鞠玉涛，常武军，周长省（2013）. NEPE固体推进剂粘-超弹性本构模型研究. 《兵工学报》.
209. 崔业兵，陈雄，周长省，姚琰，韩文超（2013）. 扰流片推力矢量控制系统动态特性研究. 《推进技术》.
210. Jian-Bin Zhang, Yu Ju, Changsheng Zhou (2013). A Study of Experimental Method for Mechanical Properties of Solid Propellant under Hydrostatic Compressive Loading.DOI
211. Jian-Bin Zhang, Yu Ju, Changsheng Zhou (2013). Experimental Research on Cohesion and Internal Friction Angle of the Double‐base Propellant.DOI
212. Changsheng Zhou (2013). Cohesive fracture investigation of HTPB propellant. Journal of Solid Rocket Technology.
213. Jin-Sheng Xu, Yu Ju, Bo Han, Changsheng Zhou, Jian-Ye Zheng (2013). Research on relaxation modulus of viscoelastic materials under unsteady temperature states based on TTSP.DOI
214. Changsheng Zhou (2013). A Visco-hyperelastic Constitutive Behaviour of NEPE Propellant. Acta Armamentarii.
215. 韩波，鞠玉涛，周长省（2012）. HTPB推进剂粘聚区本构模型反演识别研究. 《兵工学报》.
216. 朱国强，鞠玉涛，周长省，成红刚（2012）. PMMA激光点火特性研究. 《固体火箭技术》.
217. 成红刚，陈雄，鞠玉涛，周长省，朱国强（2012）. 基于热电偶动态特性的温度预估方法实验研究. 《固体火箭技术》.
218. 郑健，周长省，鞠玉涛（2012）. 弧形翼-身组合体绕流流场数值模拟及实验研究. 《南京理工大学学报》.
219. Bo Han, Yu Ju, Changsheng Zhou (2012). Simulation of crack propagation in HTPB propellant using cohesive zone model.DOI
220. Changsheng Zhou (2012). Inversion Identification of Constitutive Model of Cohesive Zone in HTPB Propellant. Acta Armamentarii.
221. Tianbo Wang, Changsheng Zhou, Yu Ju, Xiong Chen (2012). Mechanical properties with high temperature and the microstructure of carbon/phenolic ablative composites. Journal of Wuhan University of Technology-Mater. Sci. Ed..DOI
222. Jian-Bin Zhang, Yu Ju, Changsheng Zhou (2012). Research on Creep Characteristics of the Double-Base Solid Propellant.DOI
223. Bo Han, Yu Ju, Changsheng Zhou (2012). Investigation of Fracture Criterion for HTPB Propellant.DOI
224. 孟红磊，赵秀超，鞠玉涛，周长省（2011）. 基于累积损伤的双基推进剂强度准则及实验. 《推进技术》.
225. 韩波，周长省，陈雄（2011）. 固体推进剂裂纹内点火过程流固耦合数值仿真. 《固体火箭技术》.
226. 许进升，鞠玉涛，周长省，孟红磊（2011）. 变截面星孔药柱在温度冲击载荷作用下的力学特性. 《固体火箭技术》.
227. 孟亮飞，周长省（2011）. 阶梯装药火箭发动机点火升压瞬态波动特性. 《兵器装备工程学报》.
228. 张建彬，鞠玉涛，孟红磊，周长省（2011）. 改性双基推进剂药柱表面静动态应变测量方法. 《南京理工大学学报》.
229. 张磊，周长省，鞠玉涛，胡志刚（2011）. 冲压增程炮弹补燃室内铝镁推进剂燃烧流场数值模拟. 《南京理工大学学报》.
230. 孟红磊，周长省，鞠玉涛，朱国强（2010）. 非均布瞬态内压作用下星孔药柱应力分析. 《固体火箭技术》.
231. 骆晓臣，周长省，鞠玉涛（2010）. 提高固定几何二元进气道低马赫数性能的仿真研究. 《推进技术》.
232. 宋大明，周长省（2010）. 固体火箭发动机瞬态内流场数值仿真. 《弹箭与制导学报》.
233. 孟亮飞，田发林，周长省（2010）. 阶梯装药固体火箭发动机点火内流场特性研究. 《弹箭与制导学报》.
234. Changsheng Zhou (2010). Numerical Simulation of Transient Internal Flowfields in Solid Rocket Motor. Journal of Projectiles.Rockets.Missiles and Guidance.
235. 王筱蓉，姜根柱，周长省（2009）. 冲压增程弹进气道型面气动优化研究. 《固体火箭技术》.
236. 王筱蓉，姜根柱，周长省（2009）. 冲压增程炮弹流场数值仿真与分析. 《固体火箭技术》.
237. Changsheng Zhou (2009). Aerodynamic optimization research for contour of ramjet assisted projectile inlet. Journal of Solid Rocket Technology.
238. 常见虎，李军，周长省，张磊（2008）. 推力矢量发动机燃气舵舵间干扰的数值分析. 《固体火箭技术》.
239. 梁华，周长省，陈雄，于溪（2008）. 三元乙丙橡胶防热材料传热试验方法与温度数值计算. 《固体火箭技术》.
240. 李东，周长省，鞠玉涛，于溪（2008）. 双基固体推进剂药柱非线性蠕变特性实验研究. 《固体火箭技术》.
241. 王筱蓉，周长省，鞠玉涛，姜根柱（2008）. 固体火箭发动机特型喷管的型面设计. 《弹道学报》.
242. 李军，常见虎，周长省，高豫强（2008）. 推力矢量燃气舵三维气-固两相流的数值分析. 《南京理工大学学报》.
243. Xiao-Rong Wang, Gen-Zhu Jiang, Changsheng Zhou (2008). Optimization design for the two-dimensional contour of the ramjet engine inlet. 2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing.DOI
244. 陈雄，周长省，郑亚（2007）. 侧向支柱对冲压增程弹用进气道性能影响研究. 《南京理工大学学报》.
245. 常见虎，周长省，李军（2007）. 高低空环境下火箭发动机射流流场的数值分析. 《系统仿真学报》.DOI
246. 陈雄，周长省，鞠玉涛（2007）. 侧向支柱对高速旋转冲压增程弹用进气道影响的数值模拟. 《兵工学报》.
247. 鞠玉涛，周长省，朱福亚（2006）. 冲压发动机增程榴弹绕流流场数值分析. 《兵工学报》.
248. 陈雄，郑亚，周长省（2006）. 转速对高速旋转冲压增程弹用进气道影响数值模拟. 《推进技术》.
249. 赵秀超，黄克超，周长省，梁华（2006）. 火箭发动机单室双推力多孔装药设计方法. 《弹道学报》.
250. 鞠玉涛，周长省，王政时（2005）. 火箭发动机六分力试验台系统误差分析研究. 《弹箭与制导学报》.
251. 陈雄，郑亚，周长省，鞠玉涛（2005）. 冲压增程弹丸进气道复杂湍流流场数值仿真. 《兵工学报》.
252. 鞠玉涛，周长省，王政时（2005）. 超声速轴对称双锥进气道流场数值模拟研究. 《南京理工大学学报》.
253. Xiong Chen, Changsheng Zhou, Ya-Kun Zheng, Yu Ju (2005). Influence of Cowl Leading Edge on Inlet performance of Ramjet Assisted-Range Projectiles.DOI
254. Xiong Chen, Ya-Kun Zheng, Changsheng Zhou, Yu Ju (2005). Numerical Simulation on Ramjet Inlet with Different Cowl Leading Edge.DOI
255. 陈雄，周长省，郑亚（2004）. 应用TTM网格研究冲压增程弹丸进气道内外流场. 《固体火箭技术》.
256. 鞠玉涛，周长省（2001）. 弹丸湍流流场数值计算研究. 《南京理工大学学报》.
257. 陈雄，周长省，鞠玉涛（2001）. 脉冲爆震发动机性能参数计算方法. 《南京理工大学学报》.
258. 陈军，周长省，董师颜，鞠玉涛（2000）. 固体火箭发动机自动化设计系统与AutoCAD的“无缝”联结及应用. 《南京理工大学学报》.
259. 周长省，许宝庆，王政时，丘光申（1998）. 影响固体火箭发动机推力偏心特性的误差源研究. 《南京理工大学学报》.
260. Shi-Zhuo Hou, Zhen-Juan Xia, Junjie Wu, Hu Ma, Shun-Yao Liu, Changsheng Zhou. Experimental study on the combustion mechanism of rotating detonation waves with methane-rich gas in annular combustor. Fuel.DOI