Yiping Liu, H J Guo, Liu Yu, Guozhu Liang (2026). Numerical study on the vectoring performance of an aerospike nozzle with central cone deflection scheme. Aerospace Science and Technology.DOI
Weiwei Li, Yiyi Zhang, Hanyun Zheng, Yunqin He, Guozhu Liang (2026). Generative AI empowered inverse design of 3D energetic material structures for customizable combustion. Communications Engineering.DOI
Tong Shi, Yunqin He, Guozhu LIANG (2026). Study on characteristics and solution design of gas-filled accumulator in liquid rocket. Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University.DOI
Yezhen Sun, Jialin Ren, Jun Chen, Guozhu LIANG, Zhigang Wang, Liangen Xia, Xiaodong Wang (2026). Catalytic ignition for hydroxylammonium nitrate-based thruster based on gas dynamic resonance heating. Advances in Space Research.DOI
Yiyi Zhang, Wen-Tao Li, Yun-Qin He, Guozhu Liang (2026). An Auto-Decoding Finite Element-Enhanced Deep Energy Method for Parallel Structural Analysis of Complex Solid Propellants. Applied Mathematical Modelling.DOI
Lide Chao, Hongjie Guo, Yong Xu, Yunqin He, Guozhu Liang (2025). Green run test assessment of the high-altitude simulation test facility for liquid attitude and orbit control engines. Aerospace Science and Technology.DOI
Lide Chao, Hongjie Guo, Yong Xu, Yunqin He, Guozhu Liang (2025). Performance prediction method of multi-stage steam ejector system in high-altitude simulation test. AIP Advances.DOI
Tong Shi, Guozhu Liang, Yunqin He (2025). Numerical Simulation Study on the Impedance of the Communication Port of Liquid Launch Vehicle Gas-Filled Accumulators. Applied Sciences.DOI
Yezhen Sun, Sen Hu, Guozhu LIANG (2025). Establishment and Analysis of a General Mass Model for Solenoid Valves Used in Space Propulsion Systems. Mathematics.DOI
Yan Hai Xu, Hongtao Guo, Zhijin Wang, Guozhu Liang (2024). Design and simulation of an automatic tank pressurization system for ground test of small thrust LREs. IET conference proceedings..DOI
Wen-Tao Li, Wenhao Huang, Guozhu Liang (2024). On Bubble Departure Radius in Liquid Oxygen Tank of Rocket Propulsion System Under Microgravity. Chinese Journal of Space Science.DOI
Dong Li, Guozhu Liang, Yining Zhang, Hao MENG (2023). Numerical Investigation of the Effect of Inlet Total Pressure on H2/Air Non-premixed Rotating Detonation Combustor. International Bhurban Conference on Applied Sciences and Technology (IBCAST).DOI
Qifei Chen, Guozhu Liang (2022). Numerical Investigation on Particle Erosion Characteristics of the Elbow Pipe in Gas-Steam Ejection Power System. Aerospace.DOI
Wentao Li, Wenbo Li, Yunqin He, Guozhu Liang (2022). Reverse Design of Solid Propellant Grain for a Performance-Matching Goal: Shape Optimization via Evolutionary Neural Network. Aerospace.DOI
Alaa R AbdelGawad, Liang Guozhu (2022). A Numerical Simulation Study for A Dual Thrust Solid Propellant Rocket Motor Nozzle. Journal of Physics Conference Series.DOI
Shijie Liu, Guozhu Liang, Liu Ji-Chao, Yichuan Yang, Wang Hui (2021). Research on the Fatigue of Small Impulse Turbine Blade Based on the Numerical Simulation and Experimental Tests. International Journal of Aerospace Engineering.DOI
Jiachao Li, Guozhu Liang, Pingping Zhu, Xi Wang (2019). Numerical investigation of the operating process of the liquid hydrogen tank under gaseous hydrogen pressurization. Aerospace Science and Technology.DOI
Mahyar Naderi, Guozhu Liang (2019). Static performance modeling and simulation of the staged combustion cycle LPREs. Aerospace Science and Technology.DOI
Jialei Du, Guozhu Liang (2019). Dynamic coefficients and stability analysis of a water-lubricated hydrostatic bearing by solving the uncoupled Reynolds equation. Chinese Journal of Aeronautics.DOI
Jiachao Li, Guozhu Liang (2019). Simulation of mass and heat transfer in liquid hydrogen tanks during pressurizing. Chinese Journal of Aeronautics.DOI
Jialei Du, Guozhu Liang (2019). Performance comparative analysis of hydrostatic bearings lubricated with low-viscosity cryogenic fluids. Tribology International.DOI
Qiang Wei, Guozhu Liang (2019). Numerical Simulation of Ignition Process for the Monomethyl Hydrazine–Nitrogen Tetroxide Thrusters. Journal of Propulsion and Power.DOI
Jiachao Li, Guozhu Liang (2019). SIMULATION OF THE GAS AND LIQUID BEHAVIOR IN A LIQUID HYDROGEN TANK WITH A STRAIGHT PIPE INJECTOR DURING PRESSURIZATION. Interfacial phenomena and heat transfer.DOI
Walid M. Adel, Guozhu Liang (2018). Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior. Chinese Journal of Aeronautics.DOI
Zhongjian FANG, Guozhu Liang (2018). Transient simulation of a differential piston warm gas self-pressurization system for liquid attitude and divert propulsion system. Chinese Journal of Aeronautics.DOI
Walid M. Adel, Guozhu Liang (2017). Study of Cooldown Thermal Loading Effect on the Bore Deformation of Viscoelastic Solid Propellant Grain. AIAA/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Qiang Wei, Guozhu Liang (2017). Coupled Lagrangian impingement spray model for doublet impinging injectors under liquid rocket engine operating conditions. Chinese Journal of Aeronautics.DOI
Mahyar Naderi, Guozhu Liang, Hasan Karimi (2017). Modular simulation software development for liquid propellant rocket engines based on MATLAB Simulink. MATEC Web of Conferences.DOI
Yan Panyun, Liang Guozhu, LU Yongzhi, QI Zhihui, Gao Xingdou (2017). Modelling and Simulation on Multibody Dynamics for Vehicular Cold Launch Systems Based on Subsystem Synthesis Method. IOP Conference Series Materials Science and Engineering.DOI
Jiachao LI, Guozhu LIANG (2016). Numerical Simulation of Phase Change and Heat Transfer in Cryogenic Tank under the Ground Microgravity Condition. Chinese Journal of Space Science.DOI
刘士杰,梁国柱(2015). 重复使用液体火箭发动机可用度的数字仿真. 《北京航空航天大学学报》.
Zong-qi Lei, Guozhu Liang (2015). Solution of Turbine Blade Cascade Flow Using an Improved Panel Method. International Journal of Aerospace Engineering.DOI
Lie Liu, Guozhu Liang (2015). Optimization Selection of Regulated Pressurization System Schemes for Liquid Attitude and Divert Propulsion Systems. Procedia Engineering.DOI
Liang Chen, Guozhu Liang (2013). Simulation Research of Vaporization and Pressure Variation in a Cryogenic Propellant Tank at the Launch Site. Microgravity Science and Technology.DOI
Amr Elhefny, Guozhu Liang (2013). Stress and deformation of rocket gas turbine disc under different loads using finite element modelling. Propulsion and Power Research.DOI
Guozhu Liang (2013). Calculation of internal flow in pump of liquid rocket engine based on theory of relative stream surface. Journal of Aerospace Power.
Guozhu Liang (2013). Design and Analysis of a Double Nozzles Small Thrust Difference Measuring Device. Journal of Propulsion Technology.
Guozhu Liang (2012). Calculation and analysis of thermodynamic performance for nitrous oxide bipropellant engine. Journal of Rocket Propulsion.
Guozhu Liang (2012). Flow field simulation of N_2O cavitation Venturi. Journal of Aerospace Power.
Chong Wang, Liang Guozhu (2012). Numerical simulation of pressurization system with real-gas equation.DOI
Guozhu Liang (2011). Design and optimization of solid rocket motor Finocyl grain using simulated annealing. Journal of Aerospace Power.
Guozhu Liang (2011). Simulation of pressure shock during start and shutdown operation of rocket tank pressurization system. Journal of Aerospace Power.
Hongjie Guo, Guozhu Liang (2009). Theoretical and Experimental Investigation of Influence of Mixture Ratio on Hydrogen-Oxygen Detonation Characteristics. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC).DOI
Ioannis William Kokkinakis, Dimitris Drikakis, Yunqin He, Guozhu Liang (2022). Insight Into Supersonic Combustion Using High-order Simulations. Research Square.DOI
书籍章节
Yunqin He, Lili Yang, Xijie J. Wang, Xiaoli Wang, Guozhu Liang (2025). Simulation Analysis of Liquid Oxygen Effects in Hydrogen–Oxygen Torch Ignitor. Springer aerospace technology.DOI
Sen Hu, Yongzhi Wang, Wei Liu, Guozhu Liang (2025). Numerical Simulation on Flow Characteristics of the Fuel Overload Protection Valve in Liquid Ramjet. Springer aerospace technology.DOI
Wentao Li, Yunqin He, Guozhu Liang (2025). Solving the Finite Deformation of Solid Propellant Grain: A Deep Learning Energy Method for Thermo-Hyperelasticity. Springer aerospace technology.DOI