已发表成果:
WOK 论文 195 篇;中文核心 62 篇;其它论文 28 篇;专利发明 45 个;
Airfoils optimization based on deep reinforcement learning to improve the aerodynamic performance of rotors
Mach reflection of three-dimensional curved shock waves on V-shaped blunt leading edges
Three-dimensional high-order finite-volume method based on compact WENO reconstruction with hybrid unstructured grids
Numerical Study on Effects of Expansion Wave on Wedge-Stabilized Oblique Detonation Wave
Investigating the flow characteristics and thermodynamic performance of curved detonation waves
Analysis and Suppression of Thrust Trap for Turbo-Ramjet Mode Transition with the Integrated Optimal Control Method
Linear Lattice Boltzmann Flux Solver with Compact Third- Order Finite Volume Method for Acoustic Propagation Simulations on Three-Dimensional Hybrid Unstructured Grids
Nonlinear adaptive flight control system: Performance enhancement and validation
Reflection and transition of planar curved shock waves
Numerical investigations on interactions between 2D/3D conical shock wave and axisymmetric boundary layer at Ma=2.2
Aerodynamic optimization of airfoil based on deep reinforcement learning
Analytical model for curved-shock Mach reflection
Analytical model for predicting the length scale of shock/boundary layer interaction with curvature (vol 34, 111701, 2022)
Acoustic multipole source-simplified lattice Boltzmann method for simulating acoustic propagation problems
Deep-learning-based aerodynamic shape optimization of rotor airfoils to suppress dynamic stall
Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles
Nonlinear adaptive flight control system: Performance enhancement and validation
Coupling characteristic analysis and propagation direction control in hydrogen-air rotating detonation combustor with turbine
Formation and Evolution of Cellular Structures in Wedge-Induced Oblique Detonations
Automatic Landing System Design for Unmanned Fixed-Wing Vehicles via Multivariable Active Disturbance Rejection Control
Thermal insulation characteristics of high-temperature heat seals for hypersonic aero-engines
Robust gain-scheduled missile autopilot design based on multifrequency extended state observers
一种弯曲激波诱导爆震的起爆新方式
航空学报,1000-6893,2023-12-04.基于局部偏转吻切方法的背部进气高超飞行器一体化设计研究
空天技术,2097-0714,2023-10-15.不同气体模型与滑移边界模型下升力体摩阻热流预示研究
北京航空航天大学学报,1001-5965,2023-08-30.膨胀波对斜劈稳定斜爆震波特性影响的数值研究
推进技术,1001-4055,2023-06-02.膨胀波对斜劈稳定斜爆震波特性影响的数值研究
推进技术,1001-4055,2023-06-02.COVID-19疫情下高等院校科技创新变革与担当
高教学刊,2096-000X,2023-02-08.斜激波与轴对称边界层干扰的数值模拟
气体物理,2096-1642,2023-01-15.