Jing Shi, Li Zhou, Xiaobo Zhang, Zhanxue Wang (2026). Special Purpose Nozzles.DOI
Lu Bai, Wenjian Deng, Zhanxue Wang, Zh. Zhao (2026). Effect of cowl duct opening/closing on subsonic and supersonic performance of an adaptive cycle engine inlet. Aerospace Science and Technology.DOI
Xiang Gao, Zhanxue Wang, Zhenyu Tao (2026). GAESA-iFormer: a graph attention-enhanced scale-aware inverted transformer for performance characterization of aircraft engine compressors. Frontiers in Mechanical Engineering.DOI
Jianyu Xu, Li Zhou, Jie Shi, Zhanxue Wang, Hong Xiao, Hao Shi (2026). Effects of chemistry–vibration coupling in hypersonic non-equilibrium flow and infrared characteristics. Physics of Fluids.DOI
Xinye Zhang, Li Zhou, Jie Shi, Zhanxue Wang (2026). Numerical investigation on effects of divergent section expansion ratio on flow characteristics of multi-stream serpentine nozzle under various offset ratios. International Journal of Heat and Fluid Flow.DOI
Liying Jiao, Li Zhou, J D Shi, Zhanxue Wang (2026). Effect of exit aspect ratio on internal and external flow characteristics in integrated serpentine nozzles. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Dingwei Xue, Sheng Huang, Zhanxue Wang, Li Zhou, Hualin LIAO (2026). Research on stiffness interaction between design regions of serpentine nozzle under fluid-solid-thermal coupling. Aerospace Science and Technology.DOI
Zhixing Ji, Liwen Cheng, Xiao Chen, Zhanxue Wang (2026). Overall Configuration and Performance Analysis of a Turbofan Fuel Cells Hybrid Propulsion System toward Carbon-Neutral Aviation. Springer aerospace technology.DOI
Ziyu Zhang, Xiaobo Zhang, Zhanxue Wang, Feng Gui (2026). Flowpath Dimensions and Weight Estimate for an Advanced Open Rotor Engine. Springer aerospace technology.DOI
Yi Wang, Xiaobo Zhang, Zhanxue Wang, Hao Wang, Feng Gui (2026). Modeling and Performance Optimization of Turboelectric Propulsion System. Springer aerospace technology.DOI
Mingxin WANG, Li ZHOU, Zhanxue WANG (2026). Deep learning-driven study on thrust deflection suppression in serpentine nozzles via blowing flow control. Chinese Journal of Aeronautics.DOI
Zinan Zhao, Zhanxue WANG, Lu Bai, Mingxin Wang, Min Qi, Li Zhou, Wenjian Deng (2026). Optimization design and flow physics of end wall contouring for aeroengine bypass duct with a large radius change-to-length ratio. Physics of Fluids.DOI
Jianyu XU, Li Zhou, Jie SHI, Zhanxue WANG, Hao Shi (2026). Investigation of plume non-equilibrium infrared radiation characteristics at different altitudes. Chinese Journal of Aeronautics.DOI
Zhixing Ji, Liwen Cheng, Alina Zainullina, Zhanxue Wang (2025). Performance analysis and design of solid oxide cells system for the lunar base. Energy Conversion and Management: X.DOI
Zhixing Ji, Liwen Cheng, Peifeng Sun, Zhanxue Wang (2025). Conceptual design and comprehensive study of a dual-mode engine integrated with hydrogen fuel cells and gas turbines for wide-body aircraft. International journal of hydrogen energy.DOI
Zi-Yue Zhang, Xiaobo Zhang, Zhanxue Wang, Feng Gui (2025). Thermal cycle analysis of the detonation combustion aero-engine. Gas Turbine Experiment and Research.DOI
Wang Hao, Xiaobo Zhang, Baokuo Li, Zhanxue Wang, Dawei Li (2025). A Combined Optimization Method for the Transition Control Schedules of Aero-Engines. Aerospace.DOI
Dasheng Xiao, Aiyang Yu, Shuo Song, Hong Xiao, Zhanxue Wang (2025). Engineformer: A digital twin model for predicting aero-engine performance and degradation. Advanced Engineering Informatics.DOI
Xiangzhi Wei, Jingwei Shi, Li Zhou, Zhonghao Hui, Mingcong Miao, Zhanxue Wang (2025). Three-dimensional flow features of under-expanded jets from serpentine nozzle using background-oriented schlieren tomography. Chinese Journal of Aeronautics.DOI
Qiulin LI, Li Zhou, Jingwei Shi, Zhanxue Wang (2025). Approximate modeling and optimization design of serpentine nozzle structural displacement based on multi-physics coupling. Chinese Journal of Aeronautics.DOI
Bai Lu, Wenjian Deng, Zhanxue Wang, Min Qi (2025). Effect of airframe/inlet integration on inlet performance. Physics of Fluids.DOI
Dasheng Xiao, Shuo Song, Hong Xiao, Zhanxue Wang (2025). Predicting the performance status of aero-engines using a spatio-temporal decoupled digital twin modeling method. Advanced Engineering Informatics.DOI
Jingwei Shi, Zhonghao Hui, Li Zhou, Zhanxue Wang, Yongquan Liu (2025). Experimental investigation on the cooling performance of multi-row film holes of a serpentine nozzle. Energy.DOI
Lu Bai, Wenjian Deng, Zhanxue Wang (2025). Study on the Influence of Sharp / Blunt Fuselage on the Aerodynamic Performance of Supersonic Nacelle. Proceedings - IEEE Aerospace Conference.DOI
S. T. Wu, Jingwei Shi, Li Zhou, Zhanxue Wang (2025). Study on the Flow Field Characteristics of Adaptive Aerodynamically Balance Ejector Nozzles with a Wide Working Range. Springer aerospace technology.DOI
Jingwei Shi, Zhonghao Hui, Li Zhou, Zhanxue Wang (2024). A numerical investigation on the flow characteristics and aerodynamic performances of mechanical/fluidic hybrid shock vector control nozzles. IET conference proceedings..DOI
Baokuo Li, Sheng Huang, Huaixu Yan, Xiaobo Zhang, Kun Du, Zhanxue Wang (2024). Modeling and Performance Analysis of Variable Cycle Engine with Ceramic Matrix Composite Turbine Blades. Aerospace.DOI
Zhonghao Hui, Jingwei Shi, Wentao LIN, Li Zhou, Zhanxue Wang, Yongquan Liu (2024). Experimental investigation and numerical analysis on high-efficiency shock vectoring control serpentine nozzles. Chinese Journal of Aeronautics.DOI
Liying Jiao, Li Zhou, Jingwei Shi, Zhanxue Wang (2024). Numerical investigation into the effects of aft deck angle on the flow characteristics of a serpentine nozzle. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Dasheng Xiao, Hong Xiao, Zhanxue Wang (2024). IndRNN-Based Data-Driven Modeling Integrated With Physical Knowledge for Engine Performance Monitoring. Journal of Engineering for Gas Turbines and Power.DOI
Qihang Wang, Li Zhou, Zhanxue Wang (2024). Effect of leaned blades on the aerodynamic performance of contra-rotating open rotor. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Dasheng Xiao, Hong Xiao, Hong Xiao, Rui Li, Zhanxue Wang (2024). Application of physical-structure-driven deep learning and compensation methods in aircraft engine health management. Engineering Applications of Artificial Intelligence.DOI
Zhonghao Hui, Jingwei Shi, Zhou Li, Zhanxue Wang, Xiangzhi Wei, Yongquan Liu (2024). Experimental investigation on the effects of complex pressure gradients on the film cooling effectiveness of a serpentine nozzle. Applied Thermal Engineering.DOI
Jingwei Shi, Zhonghao Hui, Li Zhou, Zhanxue Wang (2024). Investigation on the Flow Mechanism and Dynamic Response Performance of Efficient Fluidic Thrust Vectoring Serpentine Nozzle.DOI
Jingwei Shi, Zhonghao Hui, Li Zhou, Zhanxue Wang, Yongquan Liu (2024). A Numerical Investigation of Film Cooling under the Effects of Different Adverse Pressure Gradients. Aerospace.DOI
Jie Shi, Li Zhou, Jianyu Xu, Jingwei Shi, Zhanxue Wang (2024). Experimental Study on Infrared Radiation Characteristics and Matching Performance of Low-Observable Nozzles. Journal of Propulsion and Power.DOI
Jianyu Xu, Li Zhou, Jie Shi, Yubo Meng, Jingwei Shi, Zhanxue Wang (2024). Multi-objective optimization design of aerodynamic and infrared characteristics of multi-stream serpentine nozzle. Journal of Physics Conference Series.DOI
Yubo Meng, Jingwei Shi, Li Zhou, Yi Zhang, Zhanxue Wang (2024). Influences of nozzle pressure ratio on flow characteristics of serpentine multi-stream supersonic nozzle. Journal of Physics Conference Series.DOI
Mingcong Miao, Jingwei Shi, Shuang Liang, Zhanxue Wang, Li Zhou (2024). Flow field prediction of S-shaped shock vectoring nozzle with rear deck based on deep learning. Journal of Physics Conference Series.DOI
Qiulin Li, Li Zhou, Jingwei Shi, Yi Zhang, Zhanxue Wang (2024). Investigation on influence mechanism of length-to-diameter ratio on fluid-structure interaction characteristic of serpentine nozzle. Journal of Physics Conference Series.DOI
Haiyu Zhao, Zhou Li, Wenjian Deng, Zhanxue Wang (2024). Research on aerodynamic influence of contra-rotating propfan slipstream on propfan engine nacelle inlet. Journal of Physics Conference Series.DOI
Yubo Meng, Jingwei Shi, Li Zhou, Zhanxue Wang (2023). Numerical investigation on flow characteristics of multi-stream supersonic nozzle with serpentine configuration. Aerospace Science and Technology.DOI
Shiping Ma, Xiaobo Zhang, Zhanxue Wang, Tianmu Jiang (2023). Modeling, Simulation and Performance Comparison of Variable Cycle Engine Based on Object-Oriented. International Conference on Control, Automation and Systems (ICCAS).DOI
Tianmu Jiang, Xiaobo Zhang, Zhanxue Wang, Yongquan Liu, Shiping Ma (2023). Control Law Design for the STOVL Aircraft Engine Using Variable Replacement Method. International Conference on Control, Automation and Systems (ICCAS).DOI
Qihang Wang, Li Zhou, Zhanxue Wang (2023). Performance Prediction of Open Rotor Enabled by Neural Network. International Conference on Control, Automation and Systems (ICCAS).DOI
Zhixing Ji, Jiang Qin, Kunlin Cheng, Silong Zhang, Zhanxue Wang (2023). A comprehensive evaluation of ducted fan hybrid engines integrated with fuel cells for sustainable aviation. Renewable and Sustainable Energy Reviews.DOI
Xiaobo Zhang, Jianming Zhu, Wei Tang, Zhijie Yuan, Zhanxue Wang (2023). Data-driven nonlinear MIMO modeling for turbofan aeroengine control system of autonomous aircraft. Control Engineering Practice.DOI
Zhifu Lin, Hong Xiao, Xiaobo Zhang, Zhanxue Wang (2023). Thrust Prediction of Aircraft Engine Enabled by Fusing Domain Knowledge and Neural Network Model. Aerospace.DOI
Zhonghao Hui, Jingwei Shi, Li Zhou, Liying Jiao, Rui Wang, Zhanxue Wang, Yongquan Liu (2023). The influence of the adverse pressure gradient on the flow characteristics of a serpentine nozzle with film cooling. Aerospace Science and Technology.DOI
Xiaobo Zhang, Zhanxue Wang, Li Zhou (2023). An integrated modeling approach for variable cycle engine performance analysis. Journal of the Franklin Institute.DOI
Tianmu Jiang, Xiaobo Zhang, Zhanxue Wang (2023). Modeling and Control Optimization of the Shaft Driven Lift Fan Engagement. Proceedings - IEEE Aerospace Conference.DOI
Qihang Wang, Li Zhou, Zhanxue Wang (2023). The effect of sweep on performance of open rotor under different advance ratio. Proceedings - IEEE Aerospace Conference.DOI
Liying Jiao, Li Zhou, Zhanxue Wang, Jingwei Shi (2023). Influence of Bevel Section on Flow Characteristics of Double Serpentine Nozzle with Bevel. Proceedings - IEEE Aerospace Conference.DOI
Peng Sun, Li Zhou, Zhanxue Wang, Jingwei Shi (2023). Influences of geometric parameters on serpentine nozzles for turbofan. Aerospace Science and Technology.DOI
Yao Yao, Xiaobo Zhang, Mingyang Zhang, Zhanxue Wang (2022). Modeling and Cycle Parameter Matching of a High-Speed Variable Cycle Turbofan-Ramjet Engine. Journal of Engineering for Gas Turbines and Power.DOI
Qihang Wang, Li Zhou, Zhanxue Wang (2022). SURROGATE-BASED AERODYNAMIC SHAPE OPTIMIZATION OF CONTRA ROTATING OPEN ROTOR. Proceedings.DOI
Min Qi, Zhanxue Wang, Li Zhou, Wenjian Deng (2022). Study on the Flow Characteristics of Fan Coupled Nacelle Intake under Different Angle of Attack. Proceedings.DOI
Yifan Ye, Zhanxue Wang, Xiaobo Zhang (2022). Sequential ensemble multi-objective optimization algorithm and its application on the multi-working performance optimization of the variable cycle engine. Proceedings.DOI
Peng Sun, Li Zhou, Zhanxue Wang, Jingwei Shi (2021). Temperature distributions of internal flow and external jet fields of double serpentine convergent nozzle for turbofan. Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University.DOI
Xiaobo Zhang, Zhanxue Wang, Bing Xiao, Yifan Ye (2021). A neural network learning-based global optimization approach for aero-engine transient control schedule. Neurocomputing.DOI
Ye Fan, Zhanxue Wang, Xiaobo Zhang (2021). Multi-Working Point Performance Optimization of Variable Cycle Engine Based on Ensemble Radial Basis Function Neural Network. AIAA Propulsion and Energy Forum.DOI
Zhonghao Hui, Jingwei Shi, Li Zhou, Zhanxue Wang, Yongquan Liu (2021). Experimental investigation of serpentine nozzles for turbofan. Aerospace Science and Technology.DOI
Yifan Ye, Zhanxue Wang, Xiaobo Zhang (2021). Sequential ensemble optimization based on general surrogate model prediction variance and its application on engine acceleration schedule design. Chinese Journal of Aeronautics.DOI
Fu SONG, Li Zhou, Zhanxue Wang, Zhifu Lin, Jingwei Shi (2020). Integration of high-fidelity model of forward variable area bypass injector into zero-dimensional variable cycle engine model. Chinese Journal of Aeronautics.DOI
Jie Shi, Li Zhou, Zhanxue Wang, Jingwei Shi (2020). Investigation on Influence Mechanism of Wall Coating on Infrared Radiation Signature of Serpentine Nozzle.DOI
Wang Hao, Li Zhou, Xiaobo Zhang, Zhanxue Wang (2020). Acceleration Method for Evolutionary Optimization of Variable Cycle Engine.DOI
Ziyu Zhang, Li Zhou, Xiaobo Zhang, Zhanxue Wang (2020). Open Rotor Engine Cycle Modeling and Performance Assessment.DOI
X. Sun, Shan Ma, Zhanxue Wang, Jingwei Shi, Li Zhou (2020). Compressible flow characteristics in bent duct with constant flow section. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Li Zhou, Yangrui Fan, Zhanxue Wang (2020). Numerical investigation of the blockage effect caused by rim seal flow. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Yifan Ye, Zhanxue Wang, Xiaobo Zhang (2020). An optimal pointwise weighted ensemble of surrogates based on minimization of local mean square error. Structural and Multidisciplinary Optimization.DOI
Liangliang Zhou, Zhanxue Wang (2019). Numerical Investigation on the three-Dimensional Flowfield in the Single Expansion Ramp Nozzle with Passive Cavity Flow Control. Journal of Applied Fluid Mechanics.DOI
Wen Cheng, Zhanxue Wang, Li Zhou, Jingwei Shi, X. Sun (2019). Infrared signature of serpentine nozzle with engine swirl. Aerospace Science and Technology.DOI
Fan Yang, Li Zhou, Zhanxue Wang (2019). Numerical Investigation of Unsteady Interaction between Rim Seal Flow and Upstream Vane. Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University.DOI
Yangrui Fan, Li Zhou, Zhanxue Wang (2019). Unsteady numerical investigation on viscous shear loss caused by rim seal purge flow. Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy.DOI
Jingwei Shi, Zhanxue Wang, Li Zhou, X. Sun (2019). Withdrawal: Investigation on a new concept of shock vector control nozzle assisted by flashboard. AIAA SciTech Forum.DOI
Jingwei Shi, Zhanxue Wang, Li Zhou, X. Sun (2019). Investigation on a new concept of shock vector control nozzle assisted by flashboard. AIAA SciTech Forum.DOI
Hong Zhou, Xiang Gao, Zhanxue Wang, Wei Zhang (2019). The Transient Performance of FLADE Variable Cycle Engine During Mode Transition. Lecture notes in electrical engineering.DOI
Wang Hao, Zhanxue Wang, Xiaobo Zhang, Mingyang Zhang (2018). A New Design Method for Mode Transition Control Law of Variable Cycle Engine. AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Peng Sun, Li Zhou, Zhanxue Wang, X. Sun (2018). Effect of Serpentine Nozzle on Bypass Ratio of Turbofan Engine Exhaust. AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Xiaobo Zhang, Zhanxue Wang, Yi-fan Ye (2018). Optimization of Adaptive Cycle Engine Performance Based on Improved Particle Swarm Optimization. AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Wenjie Wang, Li Zhou, Zhanxue Wang, Jingwei Shi (2018). The influence of exhaust system on the performance of the high bypass ratio turbofan engine nacelle. AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Li Zhou, Zhanxue Wang, Jingwei Shi, Xiaobo Zhang (2018). Investigation on a Blockerless Cascade Thrust Reverser System Based on Response Surface Method.DOI
Sun Xiao-Lin, Zhanxue Wang, Li Zhou, Shi Jing-Wei, Cheng Wen (2017). Flow Characteristics of Double Serpentine Convergent Nozzle With Different Inlet Configuration. Journal of Engineering for Gas Turbines and Power.DOI
Zhang Xiao-bo, Zhanxue Wang (2017). Optimization of FLADE Variable Cycle Engine Performance Based on Improved Differential Evolution Algorithm.DOI
Zhang Xiao-bo, Zhanxue Wang, Shi Jing-wei (2017). A Study on Performance of Aero-Engine With Fluidic Thrust Vector Nozzle.DOI
Sun Xiao-lin, Zhanxue Wang, Li Zhou, Shi Jing-wei, Cheng Wen (2017). Internal flow and external jet characteristics of double serpentine nozzle with different aspect ratio. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Wen Cheng, Zhanxue Wang, Li Zhou, X. Sun, Jingwei Shi (2017). Influences of shield ratio on the infrared signature of serpentine nozzle. Aerospace Science and Technology.DOI
Xiaobo Zhang, Zhanxue Wang, Jingwei Shi (2017). Optimization of Cycle Parameters of Variable Cycle Engine Based on Response Surface Model. AIAA/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Jingwei Shi, Zhanxue Wang, Zhang Xiaobo, Zhou Li (2017). Investigation on a hybrid SVC nozzle and coupling performance estimation with aero-engine. AIAA/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Wen Cheng, Li Zhou, Jingwei Shi, Zhanxue Wang (2017). Numerical Investigation on the Infrared Signature of Shock Vector Controlling Nozzle. AIAA Aerospace Sciences Meeting.DOI
X. Sun, Zhanxue Wang, Li Zhou, Zengwen Liu, Jingwei Shi (2015). Influences of Design Parameters on a Double Serpentine Convergent Nozzle. Journal of Engineering for Gas Turbines and Power.DOI
Li Zhou, Zengwen Liu, Zhanxue Wang, Hua Xiao (2015). Numerical study of passive cavity control on high-pressure ratio single expansion ramp nozzle under over-expansion condition. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Li Zhou, Zengwen Liu, Zhanxue Wang (2015). Numerical study of influence of biofuels on the combustion characteristics and performance of aircraft engine system. Applied Thermal Engineering.DOI
Xiaobo Zhang, Zhanxue Wang, Li Zhou, Zengwen Liu (2015). Multidisciplinary Design Optimization on Conceptual Design of Aero-engine. International Journal of Turbo and Jet Engines.DOI
Hao Gong, Zhanxue Wang, Li Zhou, Xiaobo Zhang, Jingkai Wang (2015). Analysis on Turbine Cooling Air Bleeding of Intercooled Recuperated Turbofan Engine.DOI
X. Sun, Zhanxue Wang, Li Zhou, Jingwei Shi, Zengwen Liu (2014). Experimental and computational investigation of double serpentine nozzle. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
Hong Zhou, Zhanxue Wang, Xiaobo Zhang, Mingdong Cao (2014). Optimization of Variable Cycle Engines by Using an Improved Differential Evolution. AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC).DOI
Li Zhou, Zhanxue Wang, Zengwen Liu (2014). Investigation on Influence of Design Parameters for Tandem Cascades Diffuser Using DOE Method. Engineering Applications of Computational Fluid Mechanics.DOI
Xiaobo Zhang, Zhanxue Wang, Zengwen Liu (2013). Influence of secondary flow on aero-engine performance. Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE.DOI
Xiaobo Zhang, Zhanxue Wang, Zengwen Liu (2013). Computational investigation of rocket based combined cycle. Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE.DOI
Chunyang Liu, Zhanxue Wang, Jiaqi Wang, Fang Yin, Kong De-ying (2010). 3D numerical simulation of clamshell thrust reverser with flap deployed while landing. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
Yongsheng Wang, Zhanxue Wang, Zengwen Liu, Huimin Ma (2010). Numerical simulation of parallel turbo-ramjet combined cycle propulsion system installed performance. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
Zengwen Liu, Zhanxue Wang, Yuanhu Cai, Huimin Ma (2010). Integrated performance of hypersonic vehicle and turbine based combined cycle propulsion system. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
Hongchao Huang, Jiandong Zhang, Zhanxue Wang (2009). Computation and Analysis of Dual Nozzle Flow Fields and Infrared Radiation. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC).DOI
Jiandong Zhang, Zhanxue Wang, Yuanhu Cai (2009). Computation of an Exhaust System Flow Field and Infrared Radiation. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC).DOI
Zengwen Liu, Zhanxue Wang, Yuanhu Cai (2009). Integrated Performance Numerical Simulation of Hypersonic Vehicle and Turbine Based Combined Cycle Propulsion System. AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC).DOI
Zhanxue Wang (2009). The design and flow field simulation of single expansion ramp nozzle with variable flaps. Machinery Design and Manufacture.
Zhanxue Wang (2009). Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles. Journal of Propulsion Technology.
Zhanxue Wang (2009). Nunerical simulation for spray characteristic of like-doublet injector. Machinery Design and Manufacture.
Zhanxue Wang (2009). Design for Throat Length of Mix-Compression Supersonic Inlet with Numerical Analysis. Xi'an Jiaotong Daxue xuebao.
Zhanxue Wang (2006). A method for calculaling off-design performance of radial-inflow turbine with one-dimensional flow theory. Machinery Design and Manufacture.
Zhanxue Wang (2006). Study on the Flow Loss on Turbine Blade with Coolant Ejection. Acta Aeronautica Et Astronautica Sinica.
Zhanxue Wang (2005). A study on different loss models in axial-flow turbines based on the methed of straemline-curvature. Machinery Design and Manufacture.
Lu Bai, Wenjian Deng, Zhanxue Wang, Zinan Zhao (2026). Numerical and experimental investigation of matching characteristics for a novel adaptive cycle engine inlet featuring a cowl duct. SSRN Electronic Journal.DOI
Zhixing Ji, Zhanxue Wang, Xing-Yuan Miao (2024). Scheme Construction and Evaluation of a Closed Solid Oxide Fuel Cell Hybrid Engine for Power and Propulsion on Ships. SSRN Electronic Journal.DOI
Zhifu Lin, Hong Xiao, Xiaobo Zhang, Zhanxue Wang (2023). Integrating Domain Knowledge with Neural Networks for Analytical Redundancy in Aircraft Engine Sensors. SSRN Electronic Journal.DOI
书籍章节
Jingwei Shi, Li Zhou, Xiaobo Zhang, Zhanxue Wang (2026). Concept and Parameter Definition of Nozzles. Springer eBooks.DOI
Jingwei Shi, Li Zhou, X. B. Zhang, Zhanxue Wang (2026). Study on the Influence of Infrared Radiation Characteristics of Serpentine Nozzles. Springer eBooks.DOI
Jingwei Shi, Li Zhou, Xiaobo Zhang, Zhanxue Wang (2026). Design Method and Flow Characterization of S-Shaped Nozzle. Springer eBooks.DOI
Jingwei Shi, Li Zhou, Xiaobo Zhang, Zhanxue Wang (2026). Design Methods and Applications of Single Expansion Ramp Nozzle. Springer eBooks.DOI
Jingwei Shi, Li Zhou, Xi Zhang, Zhanxue Wang (2026). Coupled Design and Calculation of Special-Purpose Nozzles and Aero-Engine Systems. Springer eBooks.DOI