Aerodynamics evaluation and flight test of a vertical take-off and landing fixed-wing UAV with joined-wing configuration in transition flight state von Baigang, Mi

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A CFD-CSD coupling method for simulating the dynamic impact and expulsion of fragile foreign objects from the 'inlet-bypass duct' junction of a turboprop aircraft von Baigang, Mi

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NOTAM Text Analysis and Classification Based on Attention Mechanism von Mi, Baigang, Fan, Yi, Sun, Yu

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New Flow Control Techniques with Prepositioned Stationary or Vibrating Elliptical Wing at Low Speed and High Angle of Attack von Baigang, Mi, Xuan, Bai

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A novel FEM-FVM coupled method of evaluating the explosion shock wave of a thermobaric bomb on the internal and external flow characteristics of aircraft von Mi, Baigang, Bai, Xuan

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Review of Numerical Simulations on Aircraft Dynamic Stability Derivatives von Mi, Baigang, Zhan, Hao

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High-Efficiency Simulation of Dynamic Stability Derivatives Based on a Particle Swarm Optimization and Long Short-Term Memory Network (PSO-LSTM) Coupling Aerodynamic Model von Cheng, Wenqi, Mi, Baigang

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New Flow Control Optimal Design Method of Flapping Wing Coupled with a Prepositive Elliptical Wing von Xuan, Bai, Hao, Zhan, Baigang, Mi

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Study on Aerodynamic Design of the Front Auxiliary Inlet von Zhang, Junyao, Zhan, Hao, Mi, Baigang

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Aerodynamic characteristics analysis of quadrangle inlet and exhaust grille for embedded ventilation cooling system of aircraft von Wang, Limin, Huang, Heyuan, Mi, Baigang, Zhang, Xuanjia, Zhao, Meiying

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Development on Unsteady Aerodynamic Modeling Technology at High Angles of Attack von Mi, Baigang, Cheng, Shixin, Zhan, Hao, Yu, Jingyi, Wang, Yiming

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基于EHVI加点准则的DSI进气道气动/隐身多目标代理优化方法研究 von 樊华羽, 詹浩, 程诗信, 米百刚

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Aerodynamic and Stealth Integrated Design of DSI Inlet by Surrogate-Based Multi-Objective Optimization with EHVI Infill Criterion von Fan, Huayu, Zhan, Hao, Cheng, Shixin, Mi, Baigang

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Research and Application of Multi-Objective Particle Swarm Optimization Algorithm Based on α -Stable Distribution von Fan, Huayu, Zhan, Hao, Cheng, Shixin, Mi, Baigang

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A Calculation Method of Aircraft's Rolling Dynamic Derivatives Based on Quasi-steady Assumption von Mi, Baigang, Zhan, Hao, Zhu, Jun

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Unsteady Aerodynamic Modeling of A Maneuvering Aircraft Using Indicial Functions von Dan,Rao, Zhenghong,Gao, Senlin,Chen, Fang,Xu, Baigang,Mi

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Long-endurance tailstock type hybrid power vertical take-off and landing unmanned aerial vehicle and flight control method von ZHAN HAO, DENG YANGPING, MI BAIGANG

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Hybrid power double-fuselage tilting propeller vertical take-off and landing high-speed aircraft and method von ZHAN HAO, DENG YANGPING, WANG BAN, MI BAIGANG

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Variable sweepback wing folding and unfolding mechanism and method for small patrol aircraft von ZHAN HAO, DENG YANGPING, MI BAIGANG

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Mixed multi-channel radio frequency signal sampling and processing system von ZHAN HAO, MI BAIGANG, CHEN HUIQIANG

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