蔡国飙

期刊论文

1. 戚亚群，金平，彭祺擘，张海联，蔡国飙（2026）. 基于模型的空间推进系统故障模式及影响分析方法. 《载人航天》.
2. Jie Fang, Yu-Fan Xu, Kaiyang Li, Shuang Zou, Cheng-Xuan Liu, Tianmo Wang, Jie-Qi Li, Guobiao Cai (2026). Vibration fatigue reliability-based robust design optimization of turbine blades in rocket engines using Kriging surrogate model with sequential sampling. Structural And Multidisciplinary Optimization.DOI
3. Jiang-Ning Wang, Guang-yu Tan, Haizhou Guo, Hui Tian, Hao Zhu, Jingfei Gao, Keren Lin, Yuan-Jun Zhang, Guobiao Cai (2026). Thrust prediction for hybrid rocket motors with aerodynamic throats based on radial basis function neural networks. Scientific Reports.DOI
4. Wei-Le Xu, Xingchen Li, Hao Zhu, Wen Yao, Guobiao Cai (2026). A Hybrid Deep-Learning Framework for Solid Rocket Motor Performance Prediction Based on Mechanism Modeling and Residual Learning. IEEE Transactions on Aerospace and Electronic Systems.DOI
5. Junjie Sun, Yu-Ting Chang, Hao Zhu, Yidi Liu, Baojiang Hou, Guobiao Cai (2026). Study on Aerodynamic Characteristics and Overall Scheme Design of Multi-position Coordinated Jet for Lifting-body Vehicle. Aerospace Science and Technology.DOI
6. Wei-Le Xu, Hao Zhu, Xingchen Li, Cunyu Bao, Wei Du, Guobiao Cai, Wen Yao (2026). A physics-guided multi-task deep learning framework for flow field reconstruction and its application in turbomachinery. International Journal of Heat and Fluid Flow.DOI
7. Yuchen Zhang, Yuanjun Zhang, Guobiao Cai, Minzhang Tong, Chaoliang Mu, Hui Tian, Hao Zhu (2026). Corrigendum to “Integrated 2D two-phase flow simulation with porous media model for 98% hydrogen peroxide monopropellant thruster” [Acta Astronaut. 246 (2026) 32-48]. Acta Astronautica.DOI
8. Xiaoting Niu, Hui Tian, Haotian Zhang, Hao Zhu, Ruikai Chen, Yudong Lu, Jingfei Gao, Guobiao Cai (2026). Multi-scale interphase mass transfer and evolution of condensed-phase particles in aluminized hybrid rocket motors: A coupled PBM–Euler–Lagrange investigation. International Communications in Heat and Mass Transfer.DOI
9. Yudong Lu, Hui Tian, Jingfei Gao, Ruikai Chen, Lingen Li, Xiaoting Niu, Xiaoming Gu, Guobiao Cai (2026). Experimental investigation on liquid layer behavior and entrainment mechanism of paraffin/polyethylene wax blends as hybrid rocket fuels. Acta Astronautica.DOI
10. Qiyue Zhang, Hongtao Xie, Peng Dong, Guobiao Cai, Hui Tian, Ruizhi Li (2026). Investigation on Additive Manufactured CuCrZr Alloy Regenerative Cooling Thrust Chamber: Material Properties and Structural Mechanical Response. Advances in Astronautics.DOI
11. Hao Zhu, Haizhou Guo, Junjie Sun, Hui Tian, Yuanjun Zhang, Guobiao Cai (2026). Research on the performance enhancement of HRM in low-thrust conditions using fluidic throat secondary injection. Aerospace Science and Technology.DOI
12. Xintong Li, Hao Zhu, Guobiao Cai, Hui Tian, Yuanjun ZHANG, Chen Chen, Jian Jiang (2026). Hydrodynamic mechanisms of hydrogen peroxide gel transport in an electric pump-fed system. Chinese Journal of Aeronautics.DOI
13. Chen Chen, Guobiao Cai, Xiaoyang Hu, Guocheng Shao, Runze Zhang, Changxin Cao, Huiyan Weng, Bijiao He, Guilong Ling, Lihui Liu (2026). Optical diagnostics of liquid contamination in liquid propellant rocket engine plumes: Part I–liquid film evolution on engine walls. Aerospace Science and Technology.DOI
14. Yuchen Zhang, Yuanjun Zhang, Guobiao Cai, Minzhang Tong, Chaoliang Mu, Hui Tian, Hao Zhu (2026). Integrated 2D two-phase flow simulation with porous media model for 98% hydrogen peroxide monopropellant thruster. Acta Astronautica.DOI
15. Zeyang Xiao, Bijiao He, Lihui Liu, Yatao Chen, Kuo Li, Guobiao Cai (2026). Analysis of the effects of expansion ratio on the structure and infrared radiation characteristics of engine under-expanded plume under different altitudes. Aerospace Science and Technology.DOI
16. Yiming Ke, Hao Zhu, Shuting Wang, Yuanjun Zhang, Hui Tian, Guobiao Cai (2026). Numerical simulation and analysis of nozzle mechanical erosion in hybrid rocket motors under overload conditions. Acta Astronautica.DOI
17. Hui Xiu Jin, Ping Jin, Qibo Peng, Bijiao He, Guobiao Cai (2026). High-Load Liquid Rocket Engine Turbine: Design Optimization and Flow Loss Analysis. Journal of Engineering for Gas Turbines and Power.DOI
18. Zeyang Xiao, Bijiao He, Baiyi Zhang, Yatao Chen, Guobiao Cai, Huiyan Weng (2026). A physics-informed neural network model for viscous compressible turbulent flows simulations within a rocket engine nozzle. Aerospace Science and Technology.DOI
19. 程奥，杨丹奇，孔凡超，张家仙，金平，蔡国飙（2025）. 缩比液体火箭发动机试车台超声速射流噪声试验研究. 《载人航天》.DOI
20. 肖明阳，朱平平，朱浩，蔡国飙（2025）. 基于证据理论的固液火箭发动机不确定性量化. 《宇航总体技术》.DOI
21. 孙俊杰，朱浩，杨依峰，苏伟，李巍，蔡国飙（2025）. 流量约束下再入飞行器逆向射流减阻降热特性研究. 《2025年中国航天大会论文集》.DOI
22. Junjie Sun, Hao Zhu, Hao Li, Da-Jun Xu, Guobiao Cai (2025). Transient Data-Driven Multi-Objective Intelligent Optimization of Counterflow Jet Configuration for Reentry Vehicles. Aerospace Science and Technology.DOI
23. Junjie Sun, Hao Zhu, Haohuan Han, Da-Jun Xu, Guobiao Cai (2025). Study on the Aerodynamic Characteristics of Reentry Vehicles with Multi-Mode Combined Drag and Heat Reduction Devices. Acta Astronautica.DOI
24. Bijiao He, Ziheng Zhou, Baiyi Zhang, Huiyan Weng, Weizong Wang, Guobiao Cai (2025). Development of the fast prediction surrogate model for vacuum plume field in variable-thrust engines based on multi-decoder ConvNeXt-form network. Aerospace Science and Technology.DOI
25. Xiaoting Niu, Hui Tian, Xiaoming Gu, Ruikai Chen, Yudong Lu, Jingfei Gao, Xiangyu Meng, Guobiao Cai (2025). Detailed numerical investigation on dynamic combustion characteristics of micro-aluminized hybrid rocket and experimental verification. Chinese Journal of Aeronautics.DOI
26. Hao Zhu, Yiming Ke, Shuting Wang, Hui Tian, Guobiao Cai (2025). Uncertainty-Quantified Regression-Rate Prediction for Hybrid Rocket Motors via Bayesian Fusion. Journal of Aerospace Engineering.DOI
27. Tianwen Li, Haodong He, Nanjia Yu, Xixiang Sun, Guobiao Cai (2025). A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. Scientific Reports.DOI
28. Hui Tian, Dijun Wang, Xiaoming Gu, Ruikai Chen, Yudong Lu, Xiaoting Niu, Hao Zhu, Guobiao Cai (2025). The effects of valve response characteristics and start-up schemes for a hybrid rocket engine on the dynamic characteristics of an electric pump. Acta Astronautica.DOI
29. Lihui Liu, Guobiao Cai, Weizong Wang, Bijiao He, Peichun Amy Tsai (2025). On the maximum spreading of viscous droplets impacting flat solid surfaces. Journal of Fluid Mechanics.DOI
30. Shutao Han, Guobiao Cai, Nanjia Yu, Yang Zhang, Qilin Bao (2025). Numerical investigation of parametric effects on the partial catalytic ignition of hydrogen peroxide/kerosene in a lab-scale rocket engine. Energy Conversion and Management.DOI
31. Hao Zhu, Minzhang Tong, Yuanjun Zhang, Yuanjun Zhang, Kechen Hu, Yuchen Zhang, Yuchen Zhang, Chaoliang Mu, Hui Tian, Guobiao Cai (2025). Combustion characteristics of hypergolic solid fuel using NaBH4-embedded polyethylene wax for hydrogen peroxide hybrid rocket. Acta Astronautica.DOI
32. Hui Tian, Yudong Lu, Lingen Li, Ruikai Chen, Xiaoting Niu, Yuchen Zhang, Guobiao Cai (2025). Experimental investigation on thermal behavior and regression rate characteristics of paraffin-polyethylene wax blends as hybrid rocket fuels. Acta Astronautica.DOI
33. Yiyang Du, Lihui Liu, Chenggeng Wu, Junya Yuan, Guobiao Cai, Bijiao He (2025). The influence of chemical models on hypersonic nonequilibrium flow field characteristics in numerical simulations. Aerospace Science and Technology.DOI
34. Lihui Liu, Guobiao Cai, Bohan Jiang, Bijiao He, Peichun Amy Tsai (2025). Viscous droplets impact on rough surfaces. International Journal of Multiphase Flow.DOI
35. Haifeng Huang, Guobiao Cai, Chuanfeng Wei, Baiyi Zhang, Xiang Cui, Yongjia Zhao, Huiyan Weng, Weizong Wang, Lihui Liu, Bijiao He (2025). Efficient prediction of aerodynamic forces in rarefied flow using convolutional neural network based multi-process method. Machine Learning Science and Technology.DOI
36. Hao Zhu, Xintong Li, Yuanjun Zhang, Jincheng Wang, Hui Tian, Guobiao Cai (2025). Optimization of pump-valve combined regulation strategy for electric pump-fed system in a hybrid rocket motor. Acta Astronautica.DOI
37. Xianwei Shang, Ping Jin, Wenjun Guo, Jian Ning Xu, Guobiao Cai (2025). Dynamic characteristic comparison between 1D model and 3D flow coupling with moving part model of liquid rocket engine flow regulator. Energy.DOI
38. Shutao Han, Guobiao Cai, Nanjia Yu, Bowei Jiao, Jiaqi Li, Sihan Di (2025). Experimental and simulation investigation on partially catalyzed ignition process of hydrogen peroxide/kerosene in a lab-scale rocket engine. Acta Astronautica.DOI
39. Guobiao Cai, Yuchen Zhang, Yuchen Zhang, Yuanjun Zhang, Yuanjun Zhang, Jiaqi Tian, Hao Zhu, Hui Tian (2025). Research on the combustion and internal ballistic characteristics of paraffin-enhanced grains with dual-layer skeleton in hybrid rocket motors. Aerospace Science and Technology.DOI
40. Ping Jin, Danqi Yang, Bingyang Liu, Yushan Gao, Guobiao Cai (2025). Effects of the Weber number and structural parameters on combustion characteristics of LOX/methane liquid–liquid swirl coaxial injectors. International Journal of Heat and Fluid Flow.DOI
41. Danqi Yang, Bingyang Liu, Yaqun Qi, Ping Jin, Guobiao Cai (2025). Optimized chemical reaction mechanisms for accurate simulation of hypergolic propellant combustion.DOI
42. Xiaoting Niu, Hui Tian, Xianzhu Jiang, Yudong Lu, Ruikai Chen, Jingfei Gao, Guobiao Cai (2025). A comprehensive transient fluid-solid coupled numerical model for hybrid rocket nozzle erosion and its experimental validation. Acta Astronautica.DOI
43. Yatao Chen, Bijiao He, Lihui Liu, Zeyang Xiao, Huiyan Weng, Guobiao Cai (2025). Numerical simulation for the effects of nozzle geometry and engine thrust on vacuum plume radiation characteristics. International Journal of Heat and Mass Transfer.DOI
44. Yixin Ma, Bingyang Liu, Wei Wang, Guobiao Cai, Ping Jin (2025). Reusable Turbine Material GH4586: Stochastic Analysis and Reliability Assessment of Low‐Cycle Fatigue Life Parameters at Multiple Temperatures. Fatigue & Fracture of Engineering Materials & Structures.DOI
45. Shengfei Shang, Xiaoning Yang, Yong Yang, Guobiao Cai, Weizong Wang, Bijiao He, Baiyi Zhang (2025). Discussion on modified Sigmund sputtering formula. Journal of Physics D Applied Physics.DOI
46. Yixin Ma, Bingyang Liu, Wei Wang, Ping Jin, Hui Ming Jin, Guobiao Cai (2025). Study on low-cycle fatigue life of nickel-based superalloy GH4586 at various temperatures. Nonlinear Engineering.DOI
47. 尚现伟，秦政，金平，蔡国飙（2024）. 航天动力系统分析软件发展途径思考. 《火箭推进》.
48. 张鹏宇，翁惠焱，陈亚涛，贺碧蛟，蔡国飙（2024）. 并联火箭发动机喷流红外辐射特性数值模拟研究. 《第十三届全国流体力学学术会议摘要集（上）》.DOI
49. 李阔，翁惠焱，陈亚涛，贺碧蛟，蔡国飙（2024）. 背压对姿轨控发动机羽流红外辐射特性影响数值模拟研究. 《第十三届全国流体力学学术会议摘要集（上）》.DOI
50. 戚亚群，金平，彭祺擘，张海联，蔡国飙（2024）. 基于模型的推进系统故障识别及建模方法. 《系统工程与电子技术》.
51. 周子恒，贺碧蛟，蔡国飙，翁惠焱，王伟宗，张百一（2024）. 基于深度学习的月球着陆过程真空羽流场实时重构. 《第十三届全国流体力学学术会议》.DOI
52. 杨丹奇，卓丹晨，吴润生，金平，蔡国飙（2024）. NTO/UDMH燃烧机理构建与着火特性分析. 《火箭推进》.
53. 王珏，周闯，朱平平，俞南嘉，蔡国飙（2024）. 泵入口参数对全流量补燃循环发动机动态特性影响研究. 《宇航总体技术》.
54. Jie Fang, Xiaoyu Jia, Jiaxin Zhang, Tongyang Zhang, Guobiao Cai (2024). Experimental and theoretical study of single bubble formation at the nozzle in a liquid oxygen crossflow. International Communications in Heat and Mass Transfer.DOI
55. Xun Peng, Hao Zhu, Da-Jun Xu, Wenzhi Hao, Wei-Zong Wang, Guobiao Cai (2024). Applying Machine Learning Techniques: Uncertainty Quantification in Nonlinear Dynamics Characters Predictions via Gated Recurrent Unit-Based Reduced-Order Models. International journal of pattern recognition and artificial intelligence.DOI
56. Junjie Sun, Hao Zhu, Haizhou Guo, Da-Jun Xu, Guobiao Cai (2024). Numerical Simulation and Analysis of Shoulder Jet Heat Reduction for Mechanical Deployable Reentry Vehicles. IAF Materials and Structures Symposium.DOI
57. Wei-Le Xu, Xingchen Li, Hao Zhu, Wen Yao, Yibing Liu, Guobiao Cai (2024). Thrust Prediction of Hybrid Rocket Motor Based on Physical Feature Embedding and Residual Learning. IAF Space Propulsion Symposium.DOI
58. Jia-Qi Tian, Hao Zhu, Rui-Zhi Li, Guobiao Cai (2024). Insight into HTPB pyrolysis mechanism under high-temperature: A reactive molecular dynamics study. Journal of Analytical and Applied Pyrolysis.DOI
59. Xin-Tong Li, Hao Zhu, Yuan-Jun Zhang, Jin-Cheng Wang, Guobiao Cai (2024). Optimization of Pump-Valve Combined Regulation Strategy for Electric Pump-fed System in a Hybrid Rocket Motor. IAF Space Propulsion Symposium.DOI
60. Junjie Sun, Hao Zhu, Haohuan Han, Da-Jun Xu, Guobiao Cai (2024). Optimization of Mechanical Deployable Reentry Vehicle based on Multi-Fidelity Aerodynamic-Trajectory Coupling Model. Aerospace Science and Technology.DOI
61. Haoran Shi, Jie Fang, Guobiao Cai, Nan-Jia Yu, Jiang-Ning Wang, Chuang Zhou (2024). Experimental Investigation on Pressure and Flow Regulation of Variable Area Cavitation Venturi in Pump-Feed System. IAF Space Propulsion Symposium.DOI
62. Haodong He, Tian-Wen Li, Nan-Jia Yu, Guobiao Cai, Li-Hao Zheng (2024). Optimization of Thrust Control Strategy for Electric Pump-Fed Rocket Engines. IAF Space Propulsion Symposium.DOI
63. Haizhou Guo, Hao Zhu, Junjie Sun, Yuan-Jun Zhang, Hui Tian, Guobiao Cai (2024). Fluidic Throat Technology for Hybrid Rocket Motor Based on Liquid Oxidizer Cooling. IAF Space Propulsion Symposium.DOI
64. Ping Jin, Xianwei Shang, Guobiao Cai (2024). Dynamic characteristic comparison between pressure fluctuations coupling with a moving part model of a liquid rocket engine flow regulator. Physics of Fluids.DOI
65. Ping Jin, Danqi Yang, Yushan Gao, Yongzhao Yang, Guobiao Cai (2024). Spray characteristics and combustion mechanism influence on combustion stability of UDMH/NTO pre-combustor under external excitation. International Journal of Engine Research.DOI
66. Qihan Jiang, Guobiao Cai, Lihui Liu, Junya Yuan, Chenggeng Wu, Bijiao He (2024). Effects of multiple cavities on rarefied hypersonic flows. Physics of Fluids.DOI
67. Da Gao, Guobiao Cai, Huanying Zhang, Baiyi Zhang, Lihui Liu, Bijiao He (2024). Numerical simulation of plume–surface interaction and lunar dust dispersion during lunar landing using four engines. Physics of Fluids.DOI
68. Baiyi Zhang, Guobiao Cai, Da Gao, Huiyan Weng, Weizong Wang, Bijiao He (2024). Development of convolutional neural network-based surrogate model for three-dimensional vacuum plume prediction via direct simulation Monte Carlo method. Physics of Fluids.DOI
69. Chenggeng Wu, Bijiao He, Da Gao, Chen Chen, Yatao Chen, Baiyi Zhang, Guilong Ling, Huiyan Weng, Guobiao Cai, Lihui Liu (2024). Experimental investigation and numerical simulation of intense plume impingement effects from a 10 N bipropellant thruster. Acta Astronautica.DOI
70. Hao Zhu, Xintong Li, Yuanjun Zhang, Yang Liu, Hui Tian, Guobiao Cai (2024). Trajectory/propulsion integrated design optimization of the manned lunar lander propelled by hybrid rocket motors using analytical target cascading. Acta Astronautica.DOI
71. Ping Jin, Junjie Lv, Qibo Peng, Hailian Zhang, Guobiao Cai, Jianping Zhou (2024). An analytical formula evolved from thermal-structural coupling model for life prediction and structural design of reusable thrust chambers. Applied Thermal Engineering.DOI
72. Tianfang Wei, Guobiao Cai, Huixin Tian, Yi Lu, Xiaoxiao Niu (2024). Experiment research on regression rate of aluminized solid propellant with HMX using reconstruction techniques. Journal of Physics Conference Series.DOI
73. Hui Tian, Xianzhu Jiang, Hao Zhu, Zhongshuo Wang, Guobiao Cai (2024). Effect of fuel type on spatial distribution characteristics for nozzle erosion in hybrid rocket motors. Acta Astronautica.DOI
74. Hui Tian, Xiaoting Niu, Xiangyu Meng, Xianzhu Jiang, Xiaoming Gu, Guobiao Cai (2024). Numerical and experimental investigations of micro Al particle additive on the performances of HTPB hybrid rocket motors. Acta Astronautica.DOI
75. Lap Au-Yeung, Lihui Liu, Guobiao Cai, Peichun Amy Tsai (2024). EXPERIMENTAL ANALYSIS AND MACHINE LEARNING FORECAST OF DROPLET IMPACT ON HEATED NANOSTRUCTURED SURFACE. TSpace (University of Toronto).
76. Ping Jin, Danqi Yang, Yongzhao Yang, Qibo Peng, Guobiao Cai (2024). Large eddy simulation for jet noise characteristics of liquid rocket engine with guide groove. Aerospace Science and Technology.DOI
77. Xiangyu Meng, Hui Tian, Xiaoting Niu, Hao Zhu, Jingfei Gao, Guobiao Cai (2024). Long-Duration Dynamic Numerical Simulation of Combustion and Flow in Hybrid Rocket Motors Considering Nozzle Erosion. Aerospace.DOI
78. Xiangyu Meng, Hui Tian, Xianzhu Jiang, Tianfang Wei, Guobiao Cai (2024). Experimental and numerical investigation on thermochemical erosion and mechanical erosion of carbon-based nozzles in hybrid rocket motors. Aerospace Science and Technology.DOI
79. Tianfang Wei, Guobiao Cai, Hui Tian, Xiangyu Meng, Xianzhu Jiang, Xiaoming Gu (2024). A comprehensive fluid–solid coupling dynamic simulation for spatiotemporal distribution of regression rate in hybrid rocket motors. Chinese Journal of Aeronautics.DOI
80. Shutao Han, Nanjia Yu, Guobiao Cai, Zeng Zhao (2024). Reduction of chemical mechanism and kinetics analysis for ignition of RP-3 aviation kerosene in partially catalyzed hydrogen peroxide. Fuel.DOI
81. Jiangning Wang, Guobiao Cai, Nanjia Yu, Chuang Zhou, Xiaoming Gu, Cao Li (2024). Experimental study on the internal temperature rise of a high-speed canned motor pump for liquid rocket engines. Journal of Physics Conference Series.DOI
82. Haodong He, Nanjia Yu, Sihan Di, Guobiao Cai, Chuang Zhou, Lihao Zheng (2024). Static Equilibrium Characteristics of Full‐Flow Staged Combustion Cycle Engine Under Different Propellants. International Journal of Aerospace Engineering.DOI
83. 赵胜璞，王睿青，张晓天，金平，蔡国飙（2023）. 航天器结构设计与分析软件发展. 《载人航天》.
84. 金平，吕俊杰，戚亚群，蔡国飙（2023）. 可重复使用液体火箭发动机寿命问题探讨. 《宇航总体技术》.
85. 刘思远，许健，王伟宗，蔡国飙，张金瑞（2023）. 液体火箭发动机缓冲式高压阀门关闭特性的流固耦合仿真研究. 《推进技术》.
86. Hao Zhu, Junjie Sun, Haizhou Guo, Da-Jun Xu, Guobiao Cai (2023). Research on aerodynamic shape optimization of reentry vehicle based on hybrid scale multi-fidelity neural network model. Aerospace Science and Technology.DOI
87. Hao Zhu, Haizhou Guo, Junjie Sun, Hui Tian, Guobiao Cai (2023). Research Progress on Active Secondary Jet Technology in Supersonic Flow Field of Aerospace Propulsion Systems. Fluids.DOI
88. Hao Zhu, Junjie Sun, Haizhou Guo, Da-Jun Xu, Guobiao Cai (2023). An Active Jet-Based Deployment Mechanism for Improved Aerodynamic Performance and Thermal Protection of Reentry Vehicles. Aerospace Science and Technology.DOI
89. Tian-Fang Wei, Guobiao Cai, H. Tian, Xianzhu Jiang (2023). Experiment and numerical research on regression rate of hybrid rocket motor with single-port wagon wheel fuel grain. Acta Astronautica.DOI
90. Chuang Zhou, Nan-Jia Yu, J. Ren, Guobiao Cai (2023). The influence law of the film percentage and injection on gas film cooling effect of the liquid oxygen/methane attitude control engine. Applied Thermal Engineering.DOI
91. H. Tian, Xiao-Qing Gu, Jiang-Ning Wang, Guang-yu Tan, Tong Liang, Guobiao Cai (2023). The effect of pipeline length on the transient process of an electric pump during start-up of a hybrid rocket motor. Acta Astronautica.DOI
92. Guang-yu Tan, H. Tian, Xiao-Qing Gu, Xiangyu Meng, Tian-Fang Wei, Yuan-Jun Zhang, Guobiao Cai (2023). Flow feedback control based on variable area cavitating venturi and its application in hybrid rocket motors. Acta Astronautica.DOI
93. Xiao-Qing Gu, H. Tian, Guang-yu Tan, Tong Liang, Jiang-Ning Wang, Xiangyu Meng, Guobiao Cai (2023). The filling process and its effect on the start-up of electric pump in hybrid rocket motor. Acta Astronautica.DOI
94. Wei Wang, Yixin Ma, Bing-Yang Liu, Guobiao Cai, Ping Jin (2023). Reliability analysis of reusable turbine rotor blisk: An application of parametric modelling method under multi-field coupling. Engineering Failure Analysis.DOI
95. Xianzhu Jiang, H. Tian, Guang-yu Tan, Sheng Zhao, Guobiao Cai (2023). Experiments of ablation characteristics for different nozzle materials and transient simulations on thermochemical erosion in hybrid rocket motors. Acta Astronautica.DOI
96. Tian-Fang Wei, Guobiao Cai, H. Tian, Yuan-Jun Zhang, Chengen Li, Xiangyu Meng (2023). Experimental Research on Reconstruction Techniques for Instantaneous Regression Rate of Hybrid Rocket Motor with Single-Port Wagon Wheel Fuel Grain. Aerospace.DOI
97. Yang Liu, Xintong Li, Peng-Cheng Wang, Xiaotian Zhang, Hao Zhu, Guobiao Cai (2023). Multi-Objective, Multi-Disciplinary Design Optimization and Multi-Attribute Evaluation of Hybrid Rocket Motors Used for Manned Lunar Lander. Aerospace.DOI
98. Danqi Yang, Ping Jin, Ya-Qun Qi, Guobiao Cai (2023). Effect of inlet mass flow rate oscillation on simplex swirl injector flow based on VOF-to-DPM model. Acta Astronautica.DOI
99. Jie Fang, T. Zhang, Xiaoyu Jia, Xudong Li, Jinfan Liu, Nan-Jia Yu, Chuanwei Xuan, Guobiao Cai (2023). Experimental study on the direct contact condensation of gaseous oxygen jets in crossflow of liquid oxygen. Experimental Thermal and Fluid Science.DOI
100. Tian-Fang Wei, Guobiao Cai, Guang-yu Tan (2023). Experiment research on instantaneous characteristics of variable-thrust hybrid rocket motor by reconstruction techniques. Journal of Physics, Conference Series.DOI
101. Ping Jin, Zhiwei Chen, Ji-Guo Sun, Guobiao Cai (2023). Investigation of full-scale porous injector plate transpiration cooling coupled with combustion in high-thrust H2/O2 rocket engines. Applied Thermal Engineering.DOI
102. Jiabao Xu, Yan Wu, Qingcheng Zhu, Ping Jin, Jue Wang, Guobiao Cai (2023). Transient study on filling characteristics of LOX dome. Journal of Physics, Conference Series.DOI
103. Junjie Sun, Hao Zhu, Da-Jun Xu, Guobiao Cai (2023). Aerodynamic Thermal Simulation and Heat Flux Distribution Study of Mechanical Expansion Reentry Vehicle. Aerospace.DOI
104. Xiao-Qing Gu, H. Tian, Jiang-Ning Wang, Tong Liang, Tian-Fang Wei, X. Niu, Guobiao Cai (2023). Operational instability of a high-rotational-speed electric pump in a hybrid rocket motor. Aerospace Science and Technology.DOI
105. Chuang Zhou, Nan-Jia Yu, Shuwen Wang, Sheng-Chun Han, Hao-Jie Gong, Guobiao Cai, Jue Wang (2023). The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines. Aerospace.DOI
106. Guang-yu Tan, H. Tian, Zhongshuo Wang, Zihao Guo, Jingfei Gao, Yuan-Jun Zhang, Guobiao Cai (2023). Experimental Investigation into Closed-Loop Control for HTPB-Based Hybrid Rocket Motors. Aerospace.DOI
107. Xinjie Li, Guobiao Cai, Junya Yuan, Yatao Chen, Bijiao He, Lihui Liu (2023). Influences of geometry configurations on the performance of micro-nozzles. Acta Astronautica.DOI
108. Xiangyu Meng, Hui Tian, Lingfei He, Jingfei Gao, Xiaoting Niu, Guobiao Cai (2023). Numerical and experimental research on axial injection end-burning hybrid rocket motors with polyethylene fuel. Chinese Journal of Aeronautics.DOI
109. Xiangyu Meng, Jingfei Gao, Hui Tian, Xiaoting Niu, Ruikai Chen, Guobiao Cai (2023). Study on the dynamic numerical simulation of flow and combustion in hybrid rocket motors based on a discrete phase model. Acta Astronautica.DOI
110. Yaqun Qi, Ping Jin, Zhiwei Chen, Junjie Lv, Guobiao Cai (2023). Thermal-structural analysis for reusable thrust chamber using temperature-dependent CuZr alloy model adapted to cryogenic to elevated temperature. Aerospace Science and Technology.DOI
111. Da Gao, Bijiao He, Huanying Zhang, Xiang Ren, Guobiao Cai, Lihui Liu (2023). Thermal protection of a lunar lander from multi-engine plumes using thin film cooling. Aerospace Science and Technology.DOI
112. Yuanyuan Gao, Weizong Wang, Peiran Li, Guobiao Cai (2023). Study on the plasma plume structures in a cylindrical Hall thruster. Vacuum.DOI
113. Hui Tian, Xiaoting Niu, Xianzhu Jiang, Guobiao Cai, Ruizhi Li (2023). Multiscale Investigation of Carbon Fiber Oxidation Kinetics: Bridging Atomistic Simulation and a Finite-Rate Reaction Model. The Journal of Physical Chemistry C.DOI
114. Xiangyu Meng, Hui Tian, Ruipeng Yu, Yudong Lu, Xiaoming Gu, Guang Tan, Guobiao Cai (2023). Three-dimensional numerical simulation of hybrid rocket motor based on dynamic mesh technology. Aerospace Science and Technology.DOI
115. Xiangyu Meng, Hui Tian, Xuanhong Ge, Xiaoting Niu, Yudong Lu, Guobiao Cai (2023). Dynamic Numerical Simulation of Hybrid Rocket Motors with Fuel Containing Aluminum Hydride. International Conference on Mechanical and Aerospace Engineering.DOI
116. Yaqun Qi, Ping Jin, Guobiao Cai, Ruizhi Li (2022). A Bi-stage Multi-objective Reliability-based Design Optimization Using Surrogate Model for Reusable Thrust Chambers. Reliability Engineering & System Safety, Vol. 221.DOI
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224. 张晟，金平，蔡国飙（2018）. 推力室冷却通道结构可靠性仿真及参数敏感性分析. 《航空动力学报》.
225. 羽中豪，金平，蔡国飙（2018）. 可重复使用液体火箭发动机设计参数对推力室身部棘轮应变的影响. 《载人航天》.
226. Lihui Liu, Guobiao Cai, Feng-Yi You, Xiang Ren, Hongru Zheng, Bijiao He (2018). Improving the viability and versatility of the E × B probe with an active cooling system. Review of Scientific Instruments.DOI
227. Guobiao Cai, Hongru Zheng, Lihui Liu, Xiang Ren, Bijiao He (2018). Three-dimensional particle simulation of ion thruster plume impingement. Acta Astronautica.DOI
228. Huiyan Weng, Guobiao Cai, Lihui Liu, Hongru Zheng, Sheng-Fei Shang, Bijiao He (2018). A momentum flux measuring instrument with the variable-range for exhaust plume. AIP Advances.DOI
229. Jian Dai, Guobiao Cai, Yang Zhang, Nan-Jia Yu (2018). Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector. Aerospace Science and Technology.DOI
230. Guobiao Cai, Zhenyu Tang, Xiao-qing Wei (2018). Investigation on the Interface Smoothing of Coupled N–S/DSMC Method Using Image Processing Filters. Advances in Astronautics Science and Technology.DOI
231. Yi Li, Bing Swen Sun, Jie Fang, Liang Tong, Guobiao Cai (2018). Nonlinear Dynamic Responses of A Cantilever Beam under Mixed Mode of Vibration Loads. International Conference on Mechanical and Aerospace Engineering.DOI
232. 刘然，凌桂龙，蔡国飙（2017）. 真空羽流试验设备的负压液氮系统设计. 《航天器环境工程》.
233. 陈杰，贺碧蛟，蔡国飙（2017）. 火星环绕器羽流效应仿真研究. 《载人航天》.
234. 江凡，陈阳，樊雪松，蔡国飙（2017）. 一种新颖的基于总能量守恒的化学平衡流算法. 《火箭推进》.
235. 曹彬彬，蔡国飙，田辉，朱浩（2017）. 固液火箭发动机矢量控制与喷管效率研究. 《宇航学报》.
236. 王鹏程，朱浩，蔡国飙（2017）. 面向成本的固液火箭发动机方案设计优化. 《固体火箭技术》.
237. Guobiao Cai, Bin-Bin Cao, Hao Zhu, H. Tian, Xuan Ma (2017). Parametric investigation of secondary injection in post-chamber on combustion performance for hybrid rocket motor.DOI
238. Jing Wu, M. Bitter, Guobiao Cai, Bijiao He, C. Kaehler (2017). Investigation on aerodynamic force effect of vacuum plumes using pressure-sensitive paint technique and CFD-DSMC solution.DOI
239. Jin-Peng Jiang, Jia-Wen Li, Guobiao Cai, Jue Wang, Qi Lin (2017). Effects of axial gap and nozzle distribution on aerodynamic forces of a supersonic partial-admission turbine.DOI
240. Jin-Peng Jiang, Jia-Wen Li, Guobiao Cai, Jue Wang (2017). Effects of axial gap on aerodynamic force and response of shrouded and unshrouded blade. Science China Technological Sciences.DOI
241. Hongru Zheng, Guobiao Cai, Lihui Liu, Sheng-Fei Shang, Bijiao He (2017). Three-dimensional particle simulation of back-sputtered carbon in electric propulsion test facility.DOI
242. Guobiao Cai, Chengen Li, Sheng Zhao, H. Tian (2017). Transient analysis on ignition process of catalytic hybrid rocket motor.DOI
243. Hao Zhu, H. Tian, Guobiao Cai (2017). Hybrid uncertainty-based design optimization and its application to hybrid rocket motors for manned lunar landing.DOI
244. H. Tian, Rui-Peng Yu, Hao Zhu, Jun-Feng Wu, Guobiao Cai (2017). Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor.DOI
245. Bijiao He, Guobiao Cai, Wei-Jen Su, Zhen-Yuan Tang (2017). Stable Runge-Kutta discontinuous Galerkin solver for hypersonic rarefied gaseous flow based on 2D Boltzmann kinetic model equations.DOI
246. Yang Chen, Hua-Sheng Wang, Ji-Xia Xia, Guobiao Cai, Zhen-Peng Zhang (2017). Dynamic modeling and simulation of an integral bipropellant propulsion double-valve combined test system.DOI
247. Zhe Yang, Zhenyu Tang, Guobiao Cai, Bijiao He (2017). Development of a coupled NS-DSMC method for the simulation of plume impingement effects of space thrusters. Thermophysics and Aeromechanics.DOI
248. Yi Li, Bing Swen Sun, Jie Fang, Xuefeng Liu, Liang Tong, Guobiao Cai (2017). Application of continuum damage mechanics to vibration fatigue life prediction. Fatigue & Fracture of Engineering Materials & Structures.DOI
249. 戚亚群，李家文，蔡国飙（2016）. 2吨推力液氧甲烷发动机寿命指标分配方法研究. 《中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议》.
250. 张爱文，朱浩，蔡国飙，刘勇，李小玉（2016）. 并联式固液上面级动力系统研究. 《火箭推进》.
251. 王艳，戚亚群，蔡国飙（2016）. 2吨推力液氧甲烷重复使用发动机推力室设计. 《中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议》.
252. 杨哲，蔡国飙，顾左，商圣飞（2016）. LIPS200离子推力器羽流污染地面试验研究. 《真空科学与技术学报》.
253. 张源俊，江雅娟，俞南嘉，田辉，蔡国飙（2016）. 固液火箭发动机动态特性仿真研究综述. 《中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议论文集》.
254. Ming-Xing Zhang, Guobiao Cai, Zhen-Yuan Tang, Bijiao He, Wulong Zhang, Y. Shu (2016). Experimental and Numerical Research on the Diversion Effect of a Conic Flame Deflector for a Lunar Module Ascent Stage.DOI
255. Guobiao Cai, Yuan-Jun Zhang, Peng-Fei Wang, Tian Hui, Sheng Zhao, Nan-Jia Yu (2016). Geometric effects of fuel regression rate in hybrid rocket motors. Science China Technological Sciences.DOI
256. Chengen Li, Guobiao Cai, H. Tian (2016). Numerical analysis of combustion characteristics of hybrid rocket motor with multi-section swirl injection.DOI
257. Guobiao Cai, Gui-Long Ling, Bijiao He (2016). An introduction to the novel vacuum plume effects experimental system.DOI
258. Xing-Liang Sun, H. Tian, Yue-Long Li, Nan-Jia Yu, Guobiao Cai (2016). Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor.DOI
259. Guobiao Cai, Yuan-Jun Zhang, H. Tian, Peng-Fei Wang, Nan-Jia Yu (2016). Effect of grain port length-diameter ratio on combustion performance in hybrid rocket motors.DOI
260. Guobiao Cai, Chengen Li, H. Tian (2016). Numerical and experimental analysis of heat transfer in injector plate of hydrogen peroxide hybrid rocket motor.DOI
261. Sheng-Fei Shang, Guobiao Cai, Ding-Qiang Zhu, Bijiao He (2016). Design of double-layer anti-sputtering targets for plume effects experimental system.DOI
262. Guobiao Cai, Jian Dai, Yang Zhang, Nan-Jia Yu (2016). Combustion behaviors of GO2/GH2 swirl-coaxial injector using non-intrusive optical diagnostics.DOI
263. Jian Dai, Guobiao Cai, Yang Zhang, Nan-Jia Yu (2016). Experimental investigations of coaxial injectors in a laboratory-scale rocket combustor.DOI
264. Jing Wu, Guobiao Cai, Bijiao He, Hao Zhou (2016). Experimental and numerical investigations of vacuum plume interaction for dual hydrogen/oxygen thrusters.DOI
265. Xing-Liang Sun, H. Tian, Guobiao Cai (2016). Diameter and position effect determination of diaphragm on hybrid rocket motor.DOI
266. 马树微，吴靖，贺碧蛟，蔡国飙（2015）. 氢氧发动机模型真空羽流场试验和仿真研究（英文）. 《航天器环境工程》.
267. 商圣飞，顾左，贺碧蛟，蔡国飙（2015）. 离子推力器束流密度分布模型. 《真空科学与技术学报》.
268. 袁军娅，李亮，蔡国飙（2015）. 基于数据库的三维复杂外形飞行器表面热流快速计算方法. 《导弹与航天运载技术(中英文)》.
269. 余佳，田辉，蔡国飙（2015）. 固液混合火箭发动机缩尺效应研究. 《火箭推进》.
270. Hao Zhu, Hui Tian, Guobiao Cai, Weimin Bao (2015). Uncertainty analysis and probabilistic design optimization of hybrid rocket motors for manned lunar landing.DOI
271. Xin Li, Jia-Wen Li, Jue Wang, Guobiao Cai (2015). Study on Cavitation Instabilities in a Three-Bladed Inducer.DOI
272. H. Tian, Xin-Tian Li, Guobiao Cai (2015). Ignition theory investigation and experimental research on hybrid rocket motor.DOI
273. Jian Dai, Nan-Jia Yu, Guobiao Cai (2015). Investigation of non-premixed flame combustion characters in GO2/GH2 shear coaxial injectors using non-intrusive optical diagnostics. Science China Physics Mechanics and Astronomy.DOI
274. Sheng Zhao, H. Tian, Peng-Fei Wang, Nan-Jia Yu, Guobiao Cai (2015). Steady-state coupled analysis of flowfields and thermochemical erosion of C/C nozzles in hybrid rocket motors.DOI
275. Hao Zhu, H. Tian, Guobiao Cai, Weimin Bao (2015). Uncertainty analysis and design optimization of hybrid rocket motor powered vehicle for suborbital flight.DOI
276. Wei-Jen Su, Alina A. Alexeenko, Guobiao Cai (2015). A parallel Runge–Kutta discontinuous Galerkin solver for rarefied gas flows based on 2D Boltzmann kinetic equations.DOI
277. Xin-Tian Li, H. Tian, Nan-Jia Yu, Guobiao Cai (2015). Experimental Investigation of Combustion in Axial-Injection End-Burning Hybrid Rocket Motor.DOI
278. Xing-Liang Sun, H. Tian, Nan-Jia Yu, Guobiao Cai (2015). Regression rate and combustion performance investigation of aluminum metallized HTPB/98HP hybrid rocket motor with numerical simulation.DOI
279. Sheng Zhao, Guobiao Cai, H. Tian, Nan-Jia Yu, P. Zeng (2015). Experimental Tests of Throttleable H2O2/PE Hybrid Rocket Motors.DOI
280. Yue Han, Guobiao Cai, Xu Xu, R. Bruno, Boukhalfa Abdelkrim (2014). A conditioned level-set method with block-division strategy to flame front extraction based on OH-PLIF measurements.DOI
281. 张熇，蔡国飙，许映乔，史纪鑫，刘自军（2014）. 嫦娥三号着陆器软着陆过程中羽流仿真分析及试验研究. 《中国科学:技术科学》.
282. Yue Han, Guobiao Cai, Hai-Xing Wang, R. Bruno, Boukhalfa Abdelkrim (2014). Flow characterization and dilution effects of N2 and CO2 on premixed CH4/air flames in a swirl-stabilized combustor.DOI
283. 宋佳，王伦，蔡国飙，齐霄强（2014）. 固液混合动力火箭地面发射系统时序设计. 《固体火箭技术》.
284. 孙兴亮，朱浩，田辉，俞南嘉，蔡国飙（2014）. 亚轨道飞行器的固液火箭发动机的高维多目标设计优化. 《宇航学报》.
285. 侯金丽，金平，蔡国飙（2014）. 含故障统计相依组件的多态复杂系统故障树分析. 《航空动力学报》.
286. 吴靖，张国舟，蔡国飙（2014）. 真空应用电火花点火的氢氧发动机设计与试验. 《航空动力学报》.
287. 唐振宇，贺碧蛟，蔡国飙（2014）. 解耦N-S/DSMC方法计算推力器真空羽流的边界条件研究. 《推进技术》.
288. 侯金丽，金平，蔡国飙（2014）. 基于模糊故障树和因子化分析的重复使用火箭发动机失效模式. 《航空动力学报》.
289. 马树微，王文龙，商圣飞，位立军，蔡国飙（2014）. 大口径低温泵抽速性能研究. 《真空科学与技术学报》.
290. 田辉，吴俊峰，俞南嘉，李君海，蔡国飙（2014）. 采用N2O与含金属HTPB燃料固液火箭发动机燃速试验研究（英文）. 《推进技术》.
291. 唐振宇，蔡国飙（2014）. 两种用于NS-DSMC耦合方法的连续失效参数对比. 《北京航空航天大学学报》.
292. Xin-Tian Li, H. Tian, Nan-Jia Yu, Guobiao Cai (2014). Experimental investigation of fuel regression rate in a HTPB based lab-scale hybrid rocket motor.DOI
293. Jin-Hui Yang, Tao Chen, Ping Jin, Guobiao Cai (2014). Influence of the startup and shutdown phases on the viscoplastic structural analysis of the thrust chamber wall.DOI
294. Zhen-Yuan Tang, Bijiao He, Guobiao Cai (2014). Numerical investigations of protector effect on a thruster.DOI
295. Jia Song, Guobiao Cai, Xiao-Qiang Qi (2014). Design of Portable Hybrid Rocket Control System.DOI
296. Yang Chen, Guobiao Cai, Zhen-Peng Zhang, Yu-Long Huang (2014). Multi-field coupling dynamic modeling and simulation of turbine test rig gas system. Simulation modelling practice and theory.DOI
297. He Zhang, Guobiao Cai, Ying-Qiao Xu, Ji-Xin Shi, Z. Liu (2014). Simulation and experimental study of the plume during the Chang’E-3 lunar landing.DOI
298. Nan-Jia Yu, Jian Dai, Guobiao Cai (2014). Small rocket engine test bed spraying apparatus.
299. Wei-Jen Su, Bijiao He, Guobiao Cai (2014). A stable Runge-Kutta discontinuous Galerkin solver for hypersonic rarefied gaseous flows.DOI
300. Zhen-Yuan Tang, Bijiao He, Guobiao Cai (2014). Investigation on a coupled Navier–Stokes–Direct Simulation Monte Carlo method for the simulation of plume flowfield of a conical nozzle.DOI
301. Hong-Yue Wang, M. Campanell, I. Kaganovich, Guobiao Cai (2014). Effect of asymmetric secondary emission in bounded low-collisional E × B plasma on sheath and plasma properties.DOI
302. H. Tian, P. Zeng, Nan-Jia Yu, Guobiao Cai (2014). Application of variable area cavitating venturi as a dynamic flow controller.DOI
303. H. Tian, Xin-Tian Li, Zeng Peng, Nan-Jia Yu, Guobiao Cai (2014). Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain $.DOI
304. Tao Chen, Jiawen Li, Ping Jin, Guobiao Cai (2013). Reusable rocket engine preventive maintenance scheduling using genetic algorithm. Reliability Engineering & System Safety, Vol. 114.DOI
305. Ping Jin, Mao-Jeng Li, Guobiao Cai (2013). Numerical and experimental study on shear coaxial injectors with hot hydrogen-rich gas/oxygen-rich gas and GH2/GO2.DOI
306. 周志成，王敏，李烽，蔡国飙，汤海滨（2013）. 我国通信卫星电推进技术的工程应用. 《国际太空》.
307. 王文龙，周建平，蔡国飙（2013）. 钟型喷管10N推力器冷流羽流气动力试验研究. 《空间控制技术与应用》.
308. 唐振宇，蔡国飙（2013）. 使用NS-DSMC耦合方法模拟发动机真空羽流流动. 《中国力学大会——2013论文摘要集》.
309. 苏微，Alina A.Alexeenko，蔡国飙（2013）. 使用直接求解ES-BGK模型方程的有限元方法计算微尺度振荡方腔流. 《中国力学大会——2013论文摘要集》.
310. 辛洁，蔡国飙，宋佳（2013）. 固液动力探空火箭箭载数据采集系统设计. 《航空动力学报》.
311. 陈阳，蔡国飙，马好东，高宁（2013）. 涡轮试验台燃烧装置建模与仿真(Ⅱ)仿真结果与分析. 《推进技术》.
312. 杨进慧，陈涛，金平，蔡国飙（2013）. 液体火箭发动机再生冷却槽黏塑性分析. 《计算机辅助工程》.
313. 吴俊峰，李新田，田辉，曾鹏，蔡国飙（2013）. 固液火箭发动机推进剂组合能量特性分析. 《固体火箭技术》.
314. 杨进慧，陈涛，金平，蔡国飙（2013）. 可重复使用火箭发动机再生冷却槽失效分析. 《北京航空航天大学学报》.
315. 申文涛，朱定强，石良臣，蔡国飙（2013）. 太阳同步轨道卫星光学特性. 《北京航空航天大学学报》.
316. 王虹玥，唐振宇，贺碧蛟，蔡国飙（2013）. 微波在液体火箭发动机真空羽流中的衰减. 《航空动力学报》.
317. 王鹏飞，田辉，俞南嘉，蔡国飙（2013）. 药柱含扰流板H2O2/HTPB固液火箭发动机两相流数值计算. 《航空动力学报》.
318. 王鹏飞，饶大林，田辉，蔡国飙（2013）. 燃烧室结构对固液火箭发动机燃速和性能的影响. 《航空动力学报》.
319. 凌桂龙，蔡国飙，张建华（2013）. 基于真空羽流试验的洁净真空系统设计. 《航空动力学报》.
320. 曾鹏，田辉，李新田，蔡国飙（2013）. H2O2/HTPB固液火箭发动机燃料配方正交优化设计. 《航空动力学报》.
321. 吴俊峰，田辉，李君海，俞南嘉，蔡国飙（2013）. 固液火箭发动机试验燃速的计算. 《航空动力学报》.
322. 毛晓芳，唐振宇，蔡国飙（2013）. 低压工况下10N姿控推力器燃烧室工作过程仿真. 《航空动力学报》.
323. 吴靖，孙威，蔡国飙（2013）. 内加热式N2O单组元推力器预热过程仿真与试验. 《航空动力学报》.
324. 孙兴亮，方杰，蔡国飙（2013）. 超径向可视化技术及其在火箭设计中的应用. 《航空动力学报》.
325. 李君海，俞南嘉，蔡国飙（2013）. 双工况流量调节阀的设计与试验. 《航空动力学报》.
326. 高玉闪，金平，蔡国飙（2013）. 近喷嘴区域燃烧流场可视化研究. 《推进技术》.
327. 高玉闪，金平，蔡国飙（2013）. 气氧/甲烷与气氢/气氧喷注器燃烧特性对比研究. 《推进技术》.
328. Xiaowei Wang, Yu-Shan Gao, Guobiao Cai, Hongfa Huo (2013). Wall Heat Transfer Measurements in High-Pressure Combustion Devices.DOI
329. Guobiao Cai (2013). Orthogonal optimal design of solid fuel formulation for H_2O_2/HTPB hybrid rocket motor. Journal of Aerospace Power.
330. H. Tian, Nan-Jia Yu, P. Zeng, Guobiao Cai (2013). Adjustable cavitation venturi tube for high concentration hydrogen peroxide.
331. Nan-Jia Yu, H. Tian, P. Zeng, Jun-Hai Li, Guobiao Cai (2013). Mobile test platform for low-thrust rocket engines.
332. Tian Hui, Xin-Tian Li, Nan-Jia Yu, Guobiao Cai (2013). Numerical and experimental investigation on the effects of aft mixing chamber diaphragm in hybrid rocket motor.DOI
333. Bijiao He, Jian-Hua Zhang, Guobiao Cai (2013). Research on vacuum plume and its effects.DOI
334. Guobiao Cai (2013). Analysis of the energy characteristics of hybrid rocket motor propellant combinations. Journal of Solid Rocket Technology.
335. Guobiao Cai, Hao Zhu, D. Rao, H. Tian (2013). Optimal design of hybrid rocket motor powered vehicle for suborbital flight.DOI
336. Guobiao Cai (2013). Simulation on working process of 10 N attitude-control thruster combustion chamber at lower-pressure condition. Journal of Aerospace Power.
337. Guobiao Cai (2013). Design and experiment of two-stage flow control valve. Journal of Aerospace Power.
338. Guobiao Cai (2013). Simulation and experiment for preheating process of N_2O monopropellant thruster with inner-heater. Journal of Aerospace Power.
339. Guobiao Cai, Zeng Peng, Xin-Tian Li, H. Tian, Nan-Jia Yu (2013). Scale effect of fuel regression rate in hybrid rocket motor.DOI
340. Jun-Hai Li, Nan-Jia Yu, P. Zeng, Guobiao Cai (2013). Design and integrated simulation of a pressurized feed system of the dual-thrust hybrid rocket motor. Science China Technological Sciences.DOI
341. Tao Chen, Jin-Hui Yang, Ping Jin, Guobiao Cai (2013). Design and Analysis for Reusable Liquid Rocket Engine Chamber.DOI
342. Ping Jin, Mao-Jeng Li, Guobiao Cai (2013). Experimental study of hydrogen-rich/oxygen-rich gas–gas injectors.DOI
343. Hong-Yue Wang, M. Campanell, I. Kaganovich, A. Khrabrov, Y. Raitses, D. Sydorenko, Guobiao Cai (2013). Effects of Asymmetric Secondary Emission on Plasma Properties of ExB Discharges.
344. Guobiao Cai (2013). On the Aerodynamic Force Experiment of Vacuum Plume for 10N Bell-Shaped Thruster. Aerospace Control and Application.
345. Bijiao He, Xiao-Ying He, Ming-Xing Zhang, Guobiao Cai (2013). Plume aerodynamic effects of cushion engine in lunar landing.DOI
346. Nan-Jia Yu, Jian Dai, Guobiao Cai (2013). Oxygen supply system for engine reusing test.
347. P. Zeng, H. Tian, Nan-Jia Yu, Guobiao Cai (2013). Numerical Investigation on Flow in the Variable Area Cavitating Venturi.DOI
348. Yang Chen, Guobiao Cai, Hao Ma, Ning Gao (2013). Numerical Modeling and Simulation of Turbine Test Rig Combustion Device(II)Simulation Results and Analysis.
349. Xin-Tian Li, H. Tian, Guobiao Cai (2013). Numerical analysis of fuel regression rate distribution characteristics in hybrid rocket motors with different fuel types. Science China Technological Sciences.DOI
350. Guobiao Cai (2013). Effect of chamber structure on fuel regression rate and performance of hybrid rocket motor. Journal of Aerospace Power.
351. Xintian Li, Hui Tian, Nanjia Yu, Guobiao Cai (2013). Three-dimensional Numerical Simulation of Two-phase Flow in Hybrid Rocket Motor. AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC).DOI
352. Guobiao Cai (2013). Hyper-radial visualization and its application in launch vehicle design. Journal of Aerospace Power.
353. 蔡国飙（2012）. 高超声速飞行器技术. 《科学出版社》.
354. 韩乐，蔡国飙（2012）. 非接触光学诊断在空间模拟舱羽流场测量中的应用研究. 《载人航天》.
355. 何小英，贺碧蛟，蔡国飙（2012）. 探月过程中的粉尘干扰效应. 《载人航天》.
356. 唐振宇，侯凤龙，蔡国飙（2012）. 双组元发动机燃烧室瞬态工作过程仿真. 《推进技术》.
357. 李茂，高玉闪，陈泽，金平，蔡国飙（2012）. 同轴剪切喷嘴出口壁厚对气-气燃烧性能的影响. 《推进技术》.
358. 蔡国飙（2012）. 固液混合火箭发动机技术综述与展望. 《推进技术》.
359. 陈阳，唐振宇，蔡国飙，黄玉龙（2012）. 涡轮试验台燃烧装置建模与仿真(Ⅰ)基于混合物分数的分区模型. 《推进技术》.
360. 毛晓芳，汪凤山，杨晓红，蔡国飙（2012）. 小推力双组元姿控发动机性能研究. 《推进技术》.
361. 朱浩，孔德帅，蔡国飙（2012）. 泵压式固液火箭发动机系统仿真与优化设计. 《航空动力学报》.
362. 柯维娜，朱定强，蔡国飙（2012）. 姿控发动机羽流的可见光/近红外特性. 《航空动力学报》.
363. 申文涛，董超，朱定强，蔡国飙（2012）. 固液混合火箭发动机喷焰红外辐射特性分析. 《航空动力学报》.
364. 姜金朋，李茂，金平，蔡国飙（2012）. 气氢/气氧同轴剪切单喷嘴燃烧室壁面热流计算与分析. 《航空动力学报》.
365. 侯金丽，金平，蔡国飙（2012）. 基于敏感性分析的氧/甲烷燃烧反应简化机理. 《航空动力学报》.
366. 李新田，俞南嘉，李君海，蔡国飙（2012）. 便携式火箭发动机地面试验测量与控制系统. 《航空动力学报》.
367. 李新田，田辉，曾鹏，蔡国飙（2012）. 固液火箭发动机工作过程三维数值仿真. 《航空动力学报》.
368. 朱浩，田辉，蔡国飙（2012）. 固液推进技术在载人登月中的应用. 《北京航空航天大学学报》.
369. 柯维娜，朱定强，蔡国飙，王伟东（2012）. 飞行弹丸红外特性的地面模拟试验. 《北京航空航天大学学报》.
370. 袁军娅，蔡国飙，杨红亮，黄建栋（2012）. 高焓非平衡气动热环境的试验模拟及影响. 《实验流体力学》.
371. 王文龙，周建平，蔡国飙（2012）. 羽流效应地面模拟试验系统关键技术发展. 《航空动力学报》.
372. 杨进慧，陈涛，金平，蔡国飙（2012）. 液体火箭发动机再生冷却槽寿命预估. 《航空动力学报》.
373. 李新田，曾鹏，田辉，蔡国飙（2012）. 固液火箭发动机试验瞬时燃速分析方法. 《推进技术》.
374. 王文龙，周建平，蔡国飙（2012）. 内置式深冷泵抽速计算及数值模拟研究. 《真空科学与技术学报》.
375. Guobiao Cai (2012). System simulation and optimal design of hybrid rocket motor with pump feed system. Journal of Aerospace Power.
376. Guobiao Cai, Wei-Jen Su, Feng-Long Hou (2012). Theoretical development for DSMC local time stepping technique.DOI
377. Xiao-Ying He, Bijiao He, Guobiao Cai (2012). Simulation of two-phase plume field of liquid thruster.DOI
378. Xiaowei Wang, Guobiao Cai, Hongfa Huo (2012). Numerical study of high-pressure GO2/GH2 combustion of a single-element injector.DOI
379. Zhen-Yuan Tang, Bijiao He, Guobiao Cai (2012). Investigation on a coupled CFD/DSMC method for continuum-rarefied flows.DOI
380. Guobiao Cai, Nan-Jia Yu, Sheng Zhao, P. Zeng (2012). Hydrogen peroxide propellant filling and supercharging operating platform.
381. Guobiao Cai (2012). Development of vacuum plume effects ground simulation experimental system key technology. Journal of Aerospace Power.
382. Guobiao Cai, Wei Sun, Jie Fang, Mao-Jeng Li, Yuntian Cong, Zhe Yang (2012). Design and performance characterization of a sub-Newton N2O monopropellant thruster.DOI
383. Xiao-Ying He, Bijiao He, Guobiao Cai (2012). Simulation of rocket plume and lunar dust using DSMC method.DOI
384. Guobiao Cai (2012). Reduced mechanism for oxygen/methane combustion based on sensitivity analysis. Journal of Aerospace Power.
385. Guobiao Cai (2012). Development and Application of Hybrid Rocket Motor Technology: Overview and Prospect. Journal of Propulsion Technology.
386. Guobiao Cai (2012). Life prediction of cooling passage for reusable liquid rocket engine. Journal of Aerospace Power.
387. Guobiao Cai (2012). Analysis of infrared radiation of hybrid rocket motor exhaust plume. Journal of Aerospace Power.
388. Wen-Long Wang, Guobiao Cai, Jian-Ping Zhou (2012). Large-scale Vacuum Vessel Design and Finite Element Analysis.DOI
389. Xiaowei Wang, Gouzhou Zhang, Guobiao Cai, Hongfa Huo (2012). Pressure and Geometry Scaling of Gaseous Hydrogen/Gaseous Oxygen Shear-Coaxial Injectors.DOI
390. Wei-Jen Su, Alina A. Alexeenko, Guobiao Cai (2012). A Runge-Kutta discontinuous Galerkin solver for 2D Boltzmann model equations: Verification and analysis of computational performance. AIP Conference Proceedings.DOI
391. D. Rao, Guobiao Cai, Hao Zhu, H. Tian (2012). Design and optimization of variable thrust hybrid rocket motors for sounding rockets.DOI
392. H. Tian, Nan-Jia Yu, Xin-Tian Li, P. Zeng, Guobiao Cai (2012). Turbulence device for postcombustion chamber of hybrid rocket engine.
393. Guobiao Cai (2012). Instantaneous Fuel Regression Rate Analysis of Hybrid Rocket Motor Experiment. Journal of Propulsion Technology.
394. Guobiao Cai (2012). Portable measurement and control system of rocket motor ground experiment. Journal of Aerospace Power.
395. Ke Weina, Zhu Dingqiang, Guobiao Cai (2012). Visible/near infrared radiation characteristics of attitude-control engine exhaust plume. Journal of Aerospace Power.
396. 孙威，方杰，吴靖，蔡国飙，丛昱（2011）. 亚牛级N 2 O单组元推力器研制. 《中国化学会第五届全国化学推进剂学术会议》.
397. 王倩，何小英，蔡国飙（2011）. 0.5N模型发动机羽流撞击效应的DSMC模拟. 《载人航天》.
398. 蔡国飙，贺碧蛟（2011）. 神舟飞船平移发动机对太阳能帆板羽流效应数值模拟研究. 《载人航天》.
399. 唐振宇，蔡国飙（2011）. 姿控发动机羽流液相污染对航天器影响分析. 《载人航天》.
400. Xiao-Wei Wang, Guobiao Cai, Yu-Shan Gao (2011). Scaling of heat transfer in gas—gas injector combustor.DOI
401. Xiao-Wei Wang, Guobiao Cai, Ping Jin (2011). Scaling study of the combustion performance of gas–gas rocket injectors.DOI
402. 金平，李茂，汪小卫，李家文，蔡国飙（2011）. 全流量补燃循环发动机系统参数模型与设计(Ⅱ)参数设计. 《航空动力学报》.
403. 金平，汪小卫，李茂，蔡国飙（2011）. 基于RLV飞行过程的氢氧发动机参数设计模型. 《北京航空航天大学学报》.
404. 张建华，贺碧蛟，蔡国飙（2011）. 轴对称羽流流场数值模拟和实验验证. 《北京航空航天大学学报》.
405. 高玉闪，陈泽，李茂，蔡国飙（2011）. 同轴撞击气-气喷嘴数值模拟和实验. 《北京航空航天大学学报》.
406. 李茂，高玉闪，金平，蔡国飙（2011）. 气气喷嘴推进剂入口温度对燃烧和壁温的影响. 《北京航空航天大学学报》.
407. 金平，杜正刚，杨立军，蔡国飙（2011）. 气-气喷注器混合场流动显示. 《航空动力学报》.
408. 李新田，曾鹏，田辉，蔡国飙（2011）. H2O2/HTPB缩比固液火箭发动机药柱燃速试验研究. 《固体火箭技术》.
409. 汪小卫，高玉闪，金平，蔡国飙（2011）. 气气多喷嘴推力室仿真与试验研究. 《推进技术》.
410. 金平，杜正刚，杨立军，蔡国飙（2011）. 互击式气-气喷注器混合场影响因素流动显示. 《推进技术》.
411. 何小英，贺碧蛟，蔡国飙（2011）. 直接模拟蒙特卡罗羽流模拟的两相作用模型. 《推进技术》.
412. 高玉闪，李茂，金平，蔡国飙（2011）. 气氧旋流强度对气-气喷嘴燃烧特性的影响. 《推进技术》.
413. 蔡国飙（2011）. 液体火箭发动机设计. 《北京航空航天大学出版社》.
414. 李茂，韩乐，方杰，孙威，蔡国飙（2011）. N2O单组元微推力器高空模拟实验研究. 《推进技术》.
415. 王虹玥，贺碧蛟，蔡国飙（2011）. 稳态等离子体推力器羽流仿真及其对微波的衰减和相移作用. 《推进技术》.
416. 凌桂龙，王文龙，蔡国飙，张建华（2011）. 用于发动机羽流试验研究的液氦热沉设计. 《航空动力学报》.
417. 朱浩，蔡国飙（2011）. 不同药型固液火箭发动机性能特点. 《航空动力学报》.
418. 李君海，曾鹏，俞南嘉，蔡国飙（2011）. 气氧/丙烷小推力发动机设计与实验. 《航空动力学报》.
419. 韩乐，李茂，方杰，孙威，蔡国飙（2011）. N2O单组元微推力器真空试验设计与分析. 《航空动力学报》.
420. 陈涛，李茂，金平，蔡国飙（2011）. 富氢/富氧燃气气-气多喷嘴正交优化设计与分析. 《航空动力学报》.
421. 池元成，朱浩，方杰，蔡国飙（2011）. 改进粒子群优化算法在亚轨道飞行器固液混合发动机设计中的应用. 《航空动力学报》.
422. 韩乐，李茂，方杰，孙威，蔡国飙（2011）. N2O微推力器结构改进的仿真与试验分析. 《航空动力学报》.
423. 李茂，高玉闪，陈泽，金平，蔡国飙（2011）. 气氢/气氧富燃预燃室设计与试验. 《航空动力学报》.
424. 金平，杜正刚，杨立军，蔡国飙（2011）. 同轴式气-气喷注器混合场影响因素流动显示研究. 《航空动力学报》.
425. Gui-Long Ling, Wen-Long Wang, Guobiao Cai, Jian-Hua Zhang (2011). Liquid helium heat sink design for experimental study of engine's plume and vacuum effects.
426. Guobiao Cai (2011). Parametric model and design of full flow staged combustion cycle engine system for(I) engine balance characteristics. Journal of Aerospace Power.
427. Guobiao Cai (2011). DSMC Numerical Simulation on Plume Impingement Effects of 0.5N Model Thruster. Manned Spaceflight.
428. Wei-Na Ke, Guobiao Cai, Ding-Qiang Zhu, Wen-tao Shen, Jiaqi Liu, Wei-Dong Wang, Lei Yuan (2011). Ground experiment of infrared characteristics of space target. Applied Optics and Photonics China.DOI
429. Guobiao Cai (2011). Flow visualization of gas-gas injector mixing flowfield. Journal of Aerospace Power.
430. Guobiao Cai, Zheng-Gang Du, Ping Jin, Mao-Jeng Li, Yu-Shan Gao (2011). Numerical and Experimental Investigation on Dual Shear Coaxial Gas‐Gas Injector.DOI
431. Guobiao Cai (2011). Two-phase coupled model for DSMC plume simulation.
432. Guobiao Cai (2011). Design and experiment for a GH_2/GO_2 fuel-rich preburner. Journal of Aerospace Power.
433. Guobiao Cai (2011). Numerical and experimental study on multi-element gas-gas injector combustors.
434. Guobiao Cai (2011). Experimental study on burning rate of sub-scale H_2O_2/HTPB hybrid rocket motor grain.
435. Yang Chen, Guobiao Cai, Zhe Wu (2011). Modularization modeling and simulation of turbine test rig main test system.DOI
436. Jian-Hua Zhang, Bijiao He, Guobiao Cai (2011). Experimental validation for axial-symmetric plume numerical simulation.
437. Li Junhai, Peng Fei Zeng, Nanjia Yu, Guobiao Cai (2011). Design and experimental research of a gas oxygen/propane small thrust engine. Journal of Aerospace Power.
438. Guobiao Cai (2011). Effect of swirl intensity on combustion characteristic of gas-gas injector.
439. Guobiao Cai, Xiao-wei Wang, Tao Chen (2011). Method for Measurement of Single-Injector Heat Transfer Characteristics and Its Application in Studying Gas-Gas Injector Combustion Chamber.DOI
440. Guobiao Cai (2011). Simulated altitude experimental investigation for N_2O monopropellant micro-thruster.
441. Guobiao Cai (2011). Simulation and experimental analysis of structure improvement for nitrous oxide micro-thruster. Journal of Aerospace Power.
442. David Xiaowei Wang, Guobiao Cai, V. Yang (2011). Modeling Study of Hydrogen/Oxygen and n-alkane/Oxygen Counterflow Diffusion Flames.DOI
443. Xiaowei Wang, Guobiao Cai, Yu-Shan Gao, Hongfa Huo, V. Yang (2011). High flowrate injector with gaseous hydrogen and gaseous oxygen.DOI
444. Guobiao Cai (2011). Design and experimental study on high flowrate multi-element gas-gas injector chamber. Journal of Aerospace Power.
445. Han Yue, Mao Li, Jie Fang, Sun Wei, Guobiao Cai (2011). Vacuum experiment study on a N_2O monopropellant micro-thruster. Journal of Aerospace Power.
446. Xing He, Bijiao He, Guobiao Cai, Jiachun Li, Song Fu (2011). Modeling of Lunar Dust Spray Using the DSMC method. AIP conference proceedings.DOI
447. Guobiao Cai (2011). Effect of Attitude-control Engine Liquid Phase Contamination on Spacecraft. Manned Spaceflight.
448. Guobiao Cai (2011). Optimal design of hybrid rocket motor for sub-orbital vehicle based on improved particle swarm optimization. Journal of Aerospace Power.
449. Guobiao Cai (2011). Design and analysis of GH_2/GO_2 fired gas multi-injectors orthogonal optimization. Journal of Aerospace Power.
450. Ping Jin, Li Mao, Xiaowei Wang, Jiawen Li, Guobiao Cai (2011). Parametric model and design of full flow staged combustion cycle engine system for(II)parameterization design. Journal of Aerospace Power.
451. 汪小卫，蔡国飙，金平 (2010). Scaling of the flowfield in a combustion chamber with a gas-gas injector. Chinese Physics B.
452. 蔡国飙，贺碧蛟（2010）. PWS软件应用于探月着陆器羽流效应数值模拟研究. 《航天器环境工程》.
453. 李茂，高玉闪，金平，蔡国飙（2010）. 富氢/富氧燃气温度对同轴直流气-气喷嘴性能的影响. 《火箭推进》.
454. 李茂，金平，蔡国飙（2010）. 富氢/富氧燃气同轴剪切气-气喷嘴性能仿真分析. 《航空动力学报》.
455. 汪小卫，高玉闪，金平，蔡国飙（2010）. 单喷嘴大流量气-气喷注器设计与试验. 《航空动力学报》.
456. 李茂，高玉闪，金平，俞南嘉，马彬，蔡国飙（2010）. 富氢/富氧燃气气-气喷嘴热试. 《推进技术》.
457. 饶大林，郑赟韬，李新田，田辉，蔡国飙（2010）. 固液混合火箭发动机仿真与优化设计. 《推进技术》.
458. 汪小卫，金平，高玉闪，蔡国飙（2010）. 气气喷注器推力室传热特性研究. 《推进技术》.
459. 俞南嘉，张国舟，马彬，蔡国飙（2010）. 应用气动谐振点火的氢氧小发动机试验. 《推进技术》.
460. 杜正刚，高玉闪，李茂，汪小卫，蔡国飙（2010）. 同轴双剪切气-气喷嘴试验研究. 《推进技术》.
461. 郑小梅，吕浩宇，徐大军，蔡国飙（2010）. 二维超燃冲压发动机磁控进气道的数值模拟. 《推进技术》.
462. 柯维娜，朱定强，蔡国飙（2010）. 金属光谱发射率的仿真与分析. 《航空学报》.
463. 汪小卫，高玉闪，金平，蔡国飙（2010）. 单喷嘴气-气喷注器推力室燃烧流场相似性. 《航空学报》.
464. 郑小梅，吕浩宇，徐大军，蔡国飙（2010）. MHD加速器模式磁控进气道的优化设计. 《航空学报》.
465. 池元成，方杰，蔡国飙（2010）. 中心变异差分进化算法. 《系统工程与电子技术》.
466. 陈阳，蔡国飙，张振鹏，夏继霞（2010）. 双组元统一推进系统减压器稳定性仿真. 《北京航空航天大学学报》.
467. 侯凤龙，蔡国飙（2010）. 应用于DSMC方法的直角网格技术. 《北京航空航天大学学报》.
468. 杜正刚，李茂，金平，蔡国飙（2010）. 大流量气-气喷嘴响应面法优化设计. 《北京航空航天大学学报》.
469. 李茂，杜正刚，金平，蔡国飙（2010）. 富氢/富氧燃气同轴直流喷嘴燃烧过程数值模拟. 《北京航空航天大学学报》.
470. 何小英，贺碧蛟，蔡国飙（2010）. Taylor-Couette流的DSMC数值模拟. 《北京航空航天大学学报》.
471. 张建华，贺碧蛟，蔡国飙（2010）. 三维多组分羽流及其效应的数值模拟. 《北京航空航天大学学报》.
472. 侯凤龙，蔡国飙（2010）. DSMC方法的边界采样与统计技术. 《北京航空航天大学学报》.
473. 俞南嘉，蔡国飙，张国舟（2010）. 环形喷嘴气动谐振加热性能. 《北京航空航天大学学报》.
474. 徐大军，蔡国飙（2010）. 高超声速飞行器关键技术量化评估方法. 《北京航空航天大学学报》.
475. 乐川，徐大军，蔡国飙（2010）. 超声速溢流条件下二元超声速进气道附加阻力计算. 《航空动力学报》.
476. 高玉闪，杜正刚，金平，蔡国飙（2010）. 热沉式燃烧室热载分析. 《航空动力学报》.
477. 池元成，方杰，饶大林，蔡国飙（2010）. 自适应中心变异差分进化算法及其在涡轮叶型优化设计中的应用. 《航空动力学报》.
478. 汪小卫，蔡国飙（2010）. 氢/氧气-气燃烧与气-液燃烧特性对比研究. 《航空动力学报》.
479. 饶大林，李新田，田辉，蔡国飙（2010）. 基于混合优化算法的固液发动机装药优化设计. 《航空动力学报》.
480. 杜正刚，高玉闪，李茂，金平，蔡国飙（2010）. 同轴双剪切气-气喷嘴数值模拟. 《航空动力学报》.
481. 李茂，杜正刚，金平，蔡国飙（2010）. 富氢/富氧燃气同轴气-气喷嘴燃烧性能仿真与分析. 《航空动力学报》.
482. 高玉闪，杜正刚，李茂，蔡国飙（2010）. 气氢/气氧喷注器流量特性实验. 《航空动力学报》.
483. 杜正刚，李茂，高玉闪，金平，蔡国飙（2010）. 气-气推进剂氧喷嘴出口型面对特征效率的影响. 《航空动力学报》.
484. 石良臣，朱定强，徐旭，蔡国飙（2010）. 月球探测器发动机羽流辐射热流计算. 《航空动力学报》.
485. 申文涛，朱定强，蔡国飙（2010）. 中段弹道目标的温度场与红外辐射特性计算. 《宇航学报》.
486. 池元成，饶大林，方杰，蔡国飙（2010）. 多目标蚁群算法及其在固液混合火箭发动机系统优化设计中的应用. 《宇航学报》.
487. 饶大林，蔡国飙（2010）. 用于快速仿真优化的改进差分进化算法及其应用. 《宇航学报》.
488. 汪小卫，金平，蔡国飙（2010）. 气-气冷流掺混流场缩尺技术. 《航空学报》.
489. 郭颜红，蔡国飙，余西龙（2010）. 激光衰减法测量固体火箭发动机尾流粒子参数. 《固体火箭技术》.
490. Guobiao Cai (2010). Simulation of radiant heat flux of rocket engine exhaust plume on lunar detector. Journal of Aerospace Power.
491. Nan-Jia Yu, Mao-Jeng Li, Guobiao Cai, Yu-Shan Gao (2010). Hydrogen-rich /oxygen-rich gas combustion tester and test method.
492. Guobiao Cai (2010). Experimental investigation on flowrate characteristics of gaseous hydrogen/gaseous oxygen injector. Journal of Aerospace Power.
493. Wei-Na Ke, Ding-Qiang Zhu, Guobiao Cai (2010). Simulation and Analysis of Spectral Emissivity of Metals.
494. Guobiao Cai (2010). Self-adaptive center-mutation differential evolution and its application to shape optimization design of a turbine blade. Journal of Aerospace Power.
495. Nan-Jia Yu, P. Zeng, Jun-Hai Li, Guobiao Cai, Tao Chen (2010). Double-working-condition stepped flow control valve and design method of control structure thereof.
496. Wei Sun, Jie Fang, Mao-Jeng Li, Guobiao Cai (2010). Internal heating nitrous oxide monopropellant gas generator.
497. Guobiao Cai, Mao-Jeng Li, Yu-Shan Gao, Ping Jin (2010). Simulation and Experiment Research for a Hydrogen-Rich/Oxygen-Rich Shear Tricoaxial Gas-Gas Injector.DOI
498. Guobiao Cai (2010). Design and experiment of high flowrate single-element gas-gas injectors. Journal of Aerospace Power.
499. Feng-Long Hou, Guobiao Cai (2010). Cartesian grid technology applied in DSMC method.
500. Guobiao Cai (2010). Simulation of GH_2/GO_2 and GH_2/LOX combustion characteristics of shear-coaxial injectors. Journal of Aerospace Power.
501. Guobiao Cai (2010). Numerical simulation of shear dual-coaxial gas-gas injector. Journal of Aerospace Power.
502. Guobiao Cai (2010). Effect of oxidizer post pattern on characteristic efficiency for gas-gas propellants. Journal of Aerospace Power.
503. Guobiao Cai (2010). Fire test on a gas-gas injector with hydrogen-rich/oxygen-rich gas.
504. Guobiao Cai (2010). Experimental investigation for hydrogen/oxygen engine using gas dynamic resonance ignition technique.
505. Guobiao Cai (2010). Performance simulation analysis for a hydrogen-rich/oxygen-rich shear coaxial gas-gas injector. Journal of Aerospace Power.
506. Guobiao Cai, Jie Fang, Yun-Tao Zheng, X. Tong, Jun Chen, Jue Wang (2010). Optimization of System Parameters for Liquid Rocket Engines with Gas-Generator Cycles.DOI
507. Guobiao Cai (2010). Calculation of additional drag coefficient of supersonic inlet under supersonic spillage condition. Journal of Aerospace Power.
508. Na Shu, Guobiao Cai, Guo-Zhou Zhang (2010). Gas dynamic resonance performance of coaxial injector.
509. Yang Chen, Guobiao Cai, Zhen-Peng Zhang, Ji-Xia Xia (2010). Numerical simulation on dynamic stability of pressure reducing regulator in integral bipropellant propulsion system.
510. Guobiao Cai (2010). Calculation of Temperature Field and Infrared Radiation Characteristics of Midcourse Ballistic Target. Journal of Astronautics.
511. Guobiao Cai (2010). Modified Differential Evolutionary Algorithm for Fast Simulation Optimization and Its Application. Journal of Astronautics.
512. Guobiao Cai (2010). Improved Particle Swarm Optimization Algorithm Based on Niche, Crossover and Selection Operators. Jisuanji fangzhen.
513. Guobiao Cai (2010). Center mutation based differential evolution. Systems engineering and electronics.
514. Guobiao Cai (2010). Optimization of grain design for hybrid rocket engine based on hybrid optimization algorithm. Journal of Aerospace Power.
515. Guobiao Cai (2010). A Multi-Objective Ant Colony Algorithm and Its Application in System Optimization Design for Hybrid Rocket Motor. Journal of Astronautics.
516. 孙威，方杰，张佳，李乐，蔡国飙（2009）. N2O单组元推力器预热过程有限元分析. 《航空动力学报》.
517. 汪小卫，金平，蔡国飙（2009）. 一种单喷嘴推力室燃烧内流场的方法. 《北京航空航天大学学报》.
518. 郑小梅，徐大军，蔡国飙（2009）. MHD能量旁路超燃冲压发动机可行性分析. 《北京航空航天大学学报》.
519. 杜正刚，高玉闪，金平，蔡国飙（2009）. 速度比对气-气喷嘴燃烧性能的影响. 《推进技术》.
520. 徐大军，陈兵，蔡国飙，徐旭（2009）. 高超声速飞行器后体喷管三维构型设计. 《航空动力学报》.
521. 俞南嘉，蔡国飙，张国舟（2009）. 圆喷嘴气动谐振性能研究. 《航空动力学报》.
522. 李茂，金平，邬志岐，俞南嘉，蔡国飙（2009）. 全流量补燃循环发动机富氧预燃室设计与试验. 《航空动力学报》.
523. 杜正刚，高玉闪，金平，蔡国飙（2009）. 基于正交设计的气-气喷嘴数值模拟. 《航空动力学报》.
524. 蔡国飙，田辉，俞南嘉（2009）. 固液混合火箭发动机技术. 《载人航天》.
525. 郑小梅，徐大军，蔡国飙（2009）. 磁控进气道二维性能计算. 《航空动力学报》.
526. 石良臣，蔡国飙，朱定强（2009）. 空间飞行器红外光学信号的模拟. 《宇航学报》.
527. 杜正刚，高玉闪，蔡国飙（2009）. 氧压降对气-气喷注器燃烧过程的影响. 《宇航学报》.
528. 孙威，方杰，蔡国飙（2009）. N2O单组元微推进系统贮箱自增压特性. 《北京航空航天大学学报》.
529. Guobiao Cai (2009). Numerical simulation of the two-dimensional magneto-hydro-dynamic controlled inlet. Journal of Aerospace Power.
530. Wei Sun, Jie Fang, Guobiao Cai (2009). Tank self-pressurization process of N2O monopropellant micro-propulsion system.
531. Guobiao Cai (2009). Numerical simulation of gas-gas injector based on orthogonal design. Journal of Aerospace Power.
532. Jie Fang, Wei Sun, Mao-Jeng Li, Deyuan Zhang, Guobiao Cai, Yuntian Cong (2009). AN UPDATE ON BUAA NITROUS OXIDE MICRO-THRUSTER RESEARCH.DOI
533. Guobiao Cai (2009). Design and experiment research for oxygen-rich preburner of FFSC. Journal of Aerospace Power.
534. Xiao-Mei Zheng, Hao-Yu Lu, Da-Jun Xu, Guobiao Cai (2009). Parameter research of an MHD Controlled inlet.DOI
535. Guobiao Cai (2009). Finite element analysis on preheating process of N_2O monopropellant thruster. Journal of Aerospace Power.
536. Guobiao Cai (2009). The Effect of Oxygen Drop on Combustion Process Gas-Gas Injector. Journal of Astronautics.
537. Guobiao Cai (2009). Effect of velocity ratio on combustion process gas-gas injector.
538. Xiaoying Zhang, Guobiao Cai (2009). Investigation of the infrared characteristics of the rocket nozzle. IEEE Aerospace and Electronic Systems Magazine.DOI
539. Xiaowei Wang, Guobiao Cai, Yushan Gao, Ping Jin (2009). Large Flow Rate Shear-Coaxial Gas-Gas Injector. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC).DOI
540. Guobiao Cai (2009). Multi-objective Optimization Based on Ant Colony Algorithm. Jisuanji gongcheng.
541. Guobiao Cai (2009). Simulation Research of Multi-spectral Signature of Satellite. Guangdian gongcheng.
542. 陈阳，高芳，张振鹏，蔡国飙（2008）. 准一维可压缩瞬变管流的有限体积模型(Ⅰ)流场的有限体积模型. 《航空动力学报》.
543. 汪小卫，金平，杜正刚，蔡国飙（2008）. 氢/氧气-气喷注器冷流掺混与燃烧比较的仿真研究. 《航空动力学报》.
544. 陈兵，徐旭，蔡国飙（2008）. 一种求解抛物化Navier-Stokes方程的空间推进算法. 《力学学报》.
545. 朱定强，张小英，向红军，蔡国飙，张振鹏，石安华，黄洁（2008）. 固体火箭发动机喷流红外辐射实验及计算研究. 《宇航学报》.
546. 石喜勤，陈兵，徐旭，蔡国飙（2008）. 冲压发动机进气道/燃烧室/尾喷管耦合流场计算. 《推进技术》.
547. 汪小卫，金平，蔡国飙，张国舟（2008）. 单喷嘴燃烧室传热特性的测量方法. 《推进技术》.
548. 汪小卫，金平，张国舟，俞南嘉，蔡国飙（2008）. 全流量补燃循环试验发动机启动过程. 《推进技术》.
549. 张小英，蔡国飙，朱定强（2008）. 火箭发动机喷管辐射及壁温的计算研究. 《航空动力学报》.
550. 孙威，方杰，蔡国飙，丛昱（2008）. N2O单组元微推力器性能分析及试验. 《北京航空航天大学学报》.
551. 金平，俞南嘉，邬志岐，张国舟，蔡国飙（2008）. 氢氧全流量补燃循环发动机富燃预燃室试验. 《推进技术》.
552. 田辉，蔡国飙，孙再庸（2008）. N2O/HTPB固液火箭发动机喷管两相流计算. 《航空动力学报》.
553. Wei Sun, Jie Fang, Guobiao Cai, Yun-Chao Cong (2008). Performance analysis and experimental research on nitrous oxide monopropellant micro-thruster.
554. Guobiao Cai (2008). Start-up in a subscale full flow staged combustion cycle engine.
555. Guobiao Cai (2008). Finite volume model for quasi one-dimensional compressible transient pipe flow (II) Finite volume model of temperature field. Journal of Aerospace Power.
556. Guobiao Cai (2008). Inlet/combustor/nozzle coupled flow field calculation for ramjet.
557. Guobiao Cai (2008). Experimental investigation of fuel-rich preburner of hydrogen/oxygen FFSC cycle engine.
558. Guobiao Cai (2008). Investigation of the role of aziridine bonding agents on the aging of the composite solid rocket propellant(CSRP). Journal of Aerospace Power.
559. Guobiao Cai (2008). Simulation of cold flow and combustion characteristics of shear-coaxial GH_2/GO_2 injectors. Journal of Aerospace Power.
560. Lijun Yang, Minghe Ge, Zhang Meng-zheng, Qingfei Fu, Guobiao Cai (2008). Spray Characteristics of Recessed Gas-Liquid Coaxial Swirl Injector. Journal of Propulsion and Power.DOI
561. Guobiao Cai, Xiaowei Wang, Ping Jin, Zhenggang Du, Yushan Gao (2008). Experimental and Numerical Investigation of Large Mass Flow Rate Gas-Gas Injectors. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC).DOI
562. Guobiao Cai (2008). Calculation for visible radiation of midcourse target. Journal of Applied Optics.
563. 张小英，朱定强，蔡国飙（2007）. 固体火箭羽流红外特性的DOM法模拟及高度影响研究. 《宇航学报》.
564. 杜正刚，金平，杨立军，蔡国飙，张蒙正（2007）. 气-气喷注器流量特性实验研究. 《航空动力学报》.
565. 郑赟韬，蔡国飙，尘军（2007）. 用于概念设计的离心泵叶轮多目标优化. 《航空动力学报》.
566. 李东霞，徐旭，蔡国飙（2007）. 基于双流体模型的超声速两相横向喷射流场研究. 《航空动力学报》.
567. 汪小卫，金平，俞南嘉，蔡国飙（2007）. 富氧预燃室试验启动过程研究. 《航空动力学报》.
568. 郑小梅，徐大军，蔡国飙（2007）. 超燃冲压发动机性能的初步分析. 《航空学报》.
569. 张建华，贺碧蛟，蔡国飙，陈爱国，杨彦广，李震乾（2007）. 卫星姿控发动机喷管羽流撞击效应试验. 《空气动力学学报》.
570. 王元光，徐旭，陈兵，蔡国飙（2007）. 冲压发动机燃烧室燃料喷射的简化计算方法研究. 《空气动力学学报》.
571. 侯凤龙，蔡国飙（2007）. 应用于DSMC方法的二维Voronoi网格技术. 《北京航空航天大学学报》.
572. 陈兵，徐旭，蔡国飙（2007）. 基于遗传算法和空间推进方法的单壁扩张喷管优化设计研究. 《航空学报》.
573. 张小英，朱定强，蔡国飙（2007）. 计算火箭发动机尾喷管红外特性的封闭腔-净辐射法. 《固体火箭技术》.
574. Guobiao Cai, Ding-Qiang Zhu, Xiaoying Zhang (2007). Calculating the Infrared Characteristics of the Rocket Nozzle with the Narrow-Band Zone Model. IEEE Aerospace Conference.DOI
575. Nan-Jia Yu, Guobiao Cai, Guo-Zhou Zhang, Bin Ma (2007). Experimental Research of Helium Resonance Heating Surface Igniter.DOI
576. Guobiao Cai, Jie Fang, Xu Xu, Minghao Liu (2007). Performance prediction and optimization for liquid rocket engine nozzle.DOI
577. Guobiao Cai (2007). Investigation of two-phase flow in supersonic crossflow based on two-fluid method. Journal of Aerospace Power.
578. Guobiao Cai (2007). Start-up experimental research on oxidizer-rich preburner. Journal of Aerospace Power.
579. H. Tian, Guobiao Cai (2007). Computation of Nozzle Flow in a N2O/HTPB Hybrid Rocket Motor.DOI
580. Guobiao Cai, Ding-Qiang Zhu, Xiaoying Zhang (2007). Numerical simulation of the infrared radiative signatures of liquid and solid rocket plumes.DOI
581. Guobiao Cai, Xiaoying Zhang, Ding-Qiang Zhu (2007). Modeling of Radiation of Participating Media with Coupled Finite Volume Method.DOI
582. Bing Chen, Xu Xu, Guobiao Cai (2007). A Multi-Code CFD Solver for the Efficient Simulation of Ramjet/Scramjet Inlet-Engine Coupled Flowfields.DOI
583. Yuan-guang Wang, Xu Xu, Guobiao Cai (2007). Numerical simulation of model scramjet combustor flowfield.DOI
584. Guobiao Cai, Ding-Qiang Zhu, Xiaoying Zhang (2007). Coupling Simulation of Heat Transfer and Temperature of the Composite Walled Nozzle of Rocket. IEEE Aerospace Conference.DOI
585. Guobiao Cai (2007). Optimization Design of Single-expansion-ramp Nozzles Using Genetic Algorithms Based on a Parabolized Navier-Stokes Solver. Acta Aeronautica Et Astronautica Sinica.
586. Guobiao Cai (2007). A Preliminary Study on Gas Phase Vacuum Plume Deposition Contamination.
587. Feng-Long Hou, Guobiao Cai (2007). Two dimensional Voronoi grid technology applied in the DSMC method.
588. Guobiao Cai (2007). Study the Infrared Characteristics of the Solid Rocket Plume with DOM Method and the Influence of Altitude. Journal of Astronautics.
589. Guobiao Cai (2007). A Preliminary Study on Hypersonic Airbreathing Engine Performance. Acta Aeronautica Et Astronautica Sinica.
590. Guobiao Cai (2007). Calculation on infrared characteristics of rocket motor nozzle by using enclosed cavity-radiative heat flux method. Journal of Solid Rocket Technology.
591. 童晓艳，蔡国飙，尘军，王珏（2006）. 燃气发生器身部多学科设计优化. 《北京航空航天大学学报》.
592. 王元光，徐旭，蔡国飙（2006）. 自由射流超燃冲压发动机燃烧室流场对比计算研究. 《宇航学报》.
593. 田耀四，蔡国飙，朱定强，田辉（2006）. 固体火箭发动机喷流流场数值仿真. 《宇航学报》.
594. 徐大军，蔡国飙，乐川（2006）. 吸气式高超声速飞行器气动热试验研究. 《宇航学报》.
595. 俞南嘉，蔡国飙，张国舟，金平，汪小卫，李茂（2006）. 富氧预燃室初步试验研究. 《宇航学报》.
596. 王元光，徐旭，蔡国飙（2006）. 超燃冲压发动机缩比燃烧室流场数值模拟. 《航空动力学报》.
597. 朱定强，薛莲，蔡国飙，张振鹏（2006）. 轨控发动机真空流场计算. 《宇航学报》.
598. 田辉，蔡国飙，王慧玉，张振鹏（2006）. 固液混合火箭发动机燃烧室和喷管流动数值模拟. 《宇航学报》.
599. 郑韬，童晓艳，蔡国飙，尘军（2006）. 液体火箭发动机系统设计仿真与优化. 《北京航空航天大学学报》.
600. 张小英，朱定强，向红军，蔡国飙（2006）. 导弹壁温的准三维计算及红外辐射研究. 《导弹与航天运载技术(中英文)》.
601. 陈兵，徐旭，蔡国飙（2006）. 基于遗传算法和空间推进方法的高超声速进气道优化设计研究. 《宇航学报》.
602. 郑赟韬，蔡国飙，尹贵增（2006）. 液体火箭发动机离心泵叶轮的多目标优化设计. 《火箭推进》.
603. 陈兵，徐旭，蔡国飙（2006）. 用空间推进算法模拟高超声速进气道流场. 《宇航学报》.
604. 陈兵，徐旭，蔡国飙（2006）. 超声速进气道可压及不可压流动数值模拟. 《北京航空航天大学学报》.
605. 江龙，姜志国，薛斌党，朱定强，蔡国飙（2006）. 导弹目标红外场景仿真技术的研究与实现. 《宇航学报》.
606. 郑赟韬，方杰，蔡国飙（2006）. 应用于工程设计的多目标优化方法比较. 《北京航空航天大学学报》.
607. Guobiao Cai, H. Tian (2006). Numerical Simulation of the Operation Process of a Hybrid Rocket Motor.DOI
608. Kun-Mei Xu, Guobiao Cai, Yun-Tao Zheng (2006). Flow field numerical study within thrust chamber of aerospace small liquid propellant rocket engine.DOI
609. Guobiao Cai (2006). Research and Realization of Infrared Scene Simulation Technology of a Missile. Journal of Astronautics.
610. Bing Chen, Xu Xu, Guobiao Cai (2006). Single- and Multi-objective Optimization of Scramjet Components Using Genetic Algorithms Based on a Parabolized Navier-Stokes Solver.DOI
611. Guobiao Cai (2006). Analysis of Comparative Numerical Simulation of Free-jet Scramjet Combustor. Journal of Astronautics.
612. X. Tong, Guobiao Cai, Yun-Tao Zheng, Jie Fang (2006). Optimization of system parameters for gas-generator engines.DOI
613. Guobiao Cai (2006). Numerical Simulation of Hypersonic Inlet Flows Using a Parabolized Navier-Stokes Algorithm. Journal of Astronautics.
614. Jian-Hua Zhang, Bijiao He, Feng-Long Hou, Guobiao Cai, Ai-Guo Chen, Yan-Guang Yang (2006). Numerical and experimental study of plume impingement effects.DOI
615. Bing Chen, Xu Xu, Guobiao Cai (2006). A New Parabolized Navier-Stokes Algorithm and its Applications in Some Hypersonic Propulsion Aerodynamic Problems.DOI
616. Nan-Jia Yu, Guobiao Cai, Guo-Zhou Zhang (2006). Research on gas-dynamic resonance igniter for simultaneous multi-ignition of hydrogen-oxygen rocket engine.DOI
617. Da-Jun Xu, Guobiao Cai, Li-Ming Zheng, Chuan Le (2006). Aeroheating Wind Tunnel Test And Thermal Protection System Design For Hypersonic Vehicle.DOI
618. Feng-Long Hou, Jian-Hua Zhang, Bijiao He, Guobiao Cai (2006). Application of self-adaptive voronoi grid technology in dsmc method.DOI
619. 陈兵，徐旭，王元光，蔡国飙（2005）. 定几何混压式轴对称超声速进气道设计及性能计算. 《航空动力学报》.
620. 田辉，蔡国飙，王慧玉，张振鹏（2005）. 固液混合火箭发动机喷管流动计算. 《航空动力学报》.
621. 李东霞，徐旭，蔡国飙，张振鹏（2005）. 火箭发动机气体-颗粒两相流双流体模型研究. 《固体火箭技术》.
622. 许坤梅，张平，蔡国飙（2005）. 燃气源控制气流绝热热流数值模拟. 《宇航学报》.
623. 方杰，田辉，孙威，蔡国飙（2005）. 一氧化二氮单组元微推进系统的初步研究. 《中国宇航学会2005年固体火箭推进第22届年会》.
624. 王元光，徐旭，蔡国飙（2005）. 超燃冲压发动机燃烧室设计计算方法的研究. 《北京航空航天大学学报》.
625. 樊士伟，张小英，朱定强，向红军，蔡国飙（2005）. 用FVM法计算固体火箭羽流的红外特性. 《宇航学报》.
626. 田辉，蔡国飙，王慧玉，张振鹏（2005）. 固液混合火箭发动机固体燃料的燃速计算. 《北京航空航天大学学报》.
627. 贺碧蛟，张建华，蔡国飙（2005）. 稳态等离子体推进器羽流场数值模拟. 《北京航空航天大学学报》.
628. 张小英，朱定强，向红军，蔡国飙（2005）. 液体火箭喷焰红外特性的数值仿真. 《北京航空航天大学学报》.
629. 方杰，田辉，蔡国飙（2005）. N2O单组元微推进系统及其喷管流场的初步研究. 《推进技术》.
630. Bijiao He, Jian-Hua Zhang, Guobiao Cai (2005). Numerical simulation of stationary plasma thruster...DOI
631. Xu Xu, Da-Jun Xu, Guobiao Cai (2005). Optimization design for scramjet and analysis of its operation performance.DOI
632. Guobiao Cai, X. Tong, Yun-Tao Zheng, Jie Fang, Jue Wang, Jun Chen (2005). Generic Optimization of System Parameters for Liquid Rocket Engine with Gas Generator Cycle.DOI
633. Guobiao Cai, Ping Jin, Li-Jun Yang, Zheng-Gang Du, Kun-Mei Xu (2005). Experimental and Numerical Investigation of Gas-Gas Injectors for Full Flow Stage Combustion Cycle Engine.DOI
634. X. Tong, Guobiao Cai, Yun-Tao Zheng, Jie Fang (2005). Optimization of System Parameters for Gas-Generato...DOI
635. Guobiao Cai (2005). Preliminary study on a N_2O micro propulsion system and its nozzle flow field.
636. Guobiao Cai (2005). Design and Performance Calculation of the Mixed-Compression Fixed-Geometry Axisymmetric Supersonic Inlets. Journal of Aerospace Power.
637. Da-Jun Xu, Xu Xu, Guobiao Cai (2005). Optimization Design for Scramjet Flowpath Consider...DOI
638. 徐旭，蔡国飙（2004）. 单模块超燃冲压发动机一体化流场数值计算. 《宇航学报》.
639. 朱定强，郑力铭，蔡国飙（2004）. 激光推进技术中激光与工质相互作用. 《北京航空航天大学学报》.
640. 方杰，童晓艳，毛晓芳，蔡国飙（2004）. 某型发动机喷管的多学科设计优化. 《推进技术》.
641. Guobiao Cai, Jian-Hua Zhang, Ai-Guo Chen, Yan-Guang Yang, China Aerodynamics (2004). Numerical and Experimental Study of Small Thruster Plume.DOI
642. Guobiao Cai (2004). Three-dimensional numerical and experimental investigation on supersonic secondary combustion.
643. 孙冰，林小树，刘小勇，蔡国飙（2003）. 硅基材料烧蚀模型研究. 《宇航学报》.
644. H. Tian, Guobiao Cai, Jian-Hua Zhang, Fu-Zhong Zhang (2003). ANALYSIS OF CZ-3A 3.RD SUBCLASS RESIDUAL PROPELLANT DISCHARGE PLUME.DOI
645. Guobiao Cai (2003). Preliminary Study of Laser Propulsion. International Astronautical Congress (IAC).DOI
646. 马朝恺，徐旭，蔡国飙（2002）. 超声速补燃的数值模拟和实验研究. 《推进技术》.
647. 陈兵，徐旭，蔡国飙（2002）. 二维超燃冲压发动机尾喷管优化设计. 《推进技术》.
648. 杨立军，胡泽保，蔡国飙，张振鹏（2002）. 溅板型层板喷注单元流量及雾化特性实验研究. 《推进技术》.
649. 张建华，蔡国飙（2002）. 用Simons法计算真空羽流. 《推进技术》.
650. 徐旭，蔡国飙（2002）. 氢/碳氢燃料超声速燃烧的数值模拟. 《推进技术》.
651. 蔡国飙，马朝恺，张化照（2002）. C-H-O-N体系液体火箭发动机喷管流场数值模拟. 《推进技术》.
652. 郑力铭，朱定强，徐旭，蔡国飙（2002）. 激光推进火箭发动机吸收室的数值模拟. 《推进技术》.
653. 田辉，蔡国飙，王慧玉，张振鹏（2002）. 固液混合火箭发动机燃烧的边界层计算. 《推进技术》.
654. 孙冰，刘小勇，林小树，蔡国飙（2002）. 固体火箭冲压发动机燃烧室热防护层烧蚀计算. 《推进技术》.
655. 陈兵，蔡国飙（2002）. 模拟真空羽流场的特征线法. 《推进技术》.
656. Guobiao Cai (2002). Method of characteristics for vacuum plume simulation.
657. 王大鹏，蔡国飙（2001）. 喷管一维流场化学非平衡通用计算软件研制. 《推进技术》.
658. 徐旭，蔡国飙（2001）. 超燃冲压发动机二维进气道优化设计方法研究. 《推进技术》.
659. 蔡国飙，郭景晶，庄逢甘，朱小兰（2001）. 考虑化学反应的真空羽流的数值模拟. 《宇航学报》.
660. Guobiao Cai, Feng-Gan Zhuang (2001). Numerical Simulation of Vacuum Plume Using Coupled-Parallel Computation.DOI
661. 蔡国飙，杜军，王慧玉，朱小兰（2000）. 真空羽流逆流污染的理论计算. 《推进技术》.
662. 蔡国飙，张化照，庄逢甘（2000）. 双组元姿控发动机喷管化学反应流场数值模拟. 《宇航学报》.
663. 蔡国飙，田辉（1999）. 旋转对固体火箭发动机的影响. 《推进技术》.
664. 蔡国飙，庄逢甘（1999）. 二维H2/O2混合和流动的直接数值模拟. 《北京航空航天大学学报》.
665. 杜军，王慧玉，蔡国飙（1999）. 真空羽流污染的数值模拟. 《北京航空航天大学学报》.
666. 蔡国飙，刘世俭，王慧玉，庄逢甘（1999）. 真空羽流场的DSMC并行数值模拟. 《航空动力学报》.
667. 高劭伦，周定，蔡国飙，庄逢甘（1999）. 低地球轨道环境原子氧对航天器表面材料聚酰亚胺作用的数值模拟. 《宇航学报》.
668. 蔡国飙，刘世俭，张振鹏（1999）. 液体火箭发动机典型实验室及典型实验概述. 《推进技术》.
669. 徐旭，蔡国飙，吕振中（1998）. 大型固体火箭发动机喷管故障诊断的流场计算. 《推进技术》.
670. 吕振中，蔡国飙，王英伟（1998）. 装药限燃包覆层脱粘和裂缝燃烧故障效应的试验研究. 《推进技术》.
671. 蔡国飙，张化照，庄逢甘（1998）. 氢氧发动机推力室化学反应流场计算. 《北京航空航天大学学报》.
672. 蔡国飙，王慧玉，庄逢甘（1998）. 真空羽流场的 N-S 和 DSMC 耦合数值模拟. 《推进技术》.
673. 蔡国飙，王慧玉，庄逢甘（1998）. 真空羽流的数值模拟及真空羽流污染的数值模拟分析研究. 《宇航学报》.
674. 蔡国飙，王慧玉，祖国君，张振鹏（1997）. 真空小喷管羽流场的Monte Carlo直接模拟. 《推进技术》.
675. 蔡国飙，孙冰，祖国君（1997）. 固体火箭发动机动力相似准则研究. 《固体火箭技术》.
676. 吕振中，王秉勋，蔡国飙，金蓉（1997）. 固体火箭发动机喷管烧穿故障的试验分析. 《推进技术》.
677. 孙冰，蔡国飙，陈全，边炳秀（1997）. 单组元发动机热回浸现象的理论分析. 《推进技术》.
678. Zhen-Zhong Lu, Bin-Xun Wang, Guobiao Cai, Yingwei Wang, Mingming Lu, Zhen-Zhong Lu, Bin-Xun Wang, Guobiao Cai, Yingwei Wang, Mingming Lu (1997). Investigation of nozzle failure in solid rocket motor. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.DOI
679. 蔡国飙，王慧玉，祖国君，张振鹏（1996）. Rayleigh问题的Monte Carlo直接模拟. 《北京航空航天大学学报》.
680. 蔡国飙. 真空羽流效应实验系统设计. 《国防工业》.
681. Wei-Le Xu, Xingchen Li, Hao Zhu, Qiao Li, Guobiao Cai, Wen Yao. Real-time rocket motor internal flow field prediction based on hybrid POD and deep neural networks. International Journal of Heat and Mass Transfer.DOI

书籍章节

1. Chuang Zhou, Nanjia Yu, Pingping Zhu, Jue Wang, Guobiao Cai, Xuesong Guo, Shan An, Haodong He (2025). Frequency Domain Analysis of Full-Flow Staged Combustion Cycle Rocket Engine System During Startup. Advances in transdisciplinary engineering.DOI
2. Jie Fang, Haoran Shi, Guobiao Cai, Nanjia Yu, Chuang Zhou, Jiangning Wang, Kang Zheng, Jieqi Li, Xiaohui Qiao (2025). Design, Testing, and Model Confidence Evaluation of High Flow Variable Area Cavitation Venturi Tube. Advances in transdisciplinary engineering.DOI
3. Da Gao, Guobiao Cai, Baiyi Zhang, Chen Chen, Bijiao He (2025). Numerical Simulation of Lunar Dust Impinged by the Engine Plume During Lunar Landing. Advances in transdisciplinary engineering.DOI
4. Danqi Yang, Bingyang Liu, Yaqun Qi, Ping Jin, Guobiao Cai (2025). Experimental and Numerical Study on the Ignition of LOX/LCH4 Liquid-Liquid Swirl Coaxial Engine. Advances in transdisciplinary engineering.DOI

数据集

1. Yufeng Cheng, Jinrui Zhang, Weizong Wang, Jiaqi Yan, Guobiao Cai（2022）. 10.1063/5.0104334.1. Default Digital Object Group.DOI