Xinglu Xia
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View article: Blade Shape Optimization and Analysis of a Propeller for VTOL Based on an Inverse Method
Blade Shape Optimization and Analysis of a Propeller for VTOL Based on an Inverse Method Open
With the rapid development of vertical takeoff and landing (VTOL) aircraft, the blade design of a propeller suitable for VTOL aircraft with a wide range of operating conditions has become a challenging and popular task. This paper proposes…
View article: Optimization and analysis of composite sandwich box beam for solar drones
Optimization and analysis of composite sandwich box beam for solar drones Open
Solar drones have garnered considerably research attention in recent years due to their continuous cruising capability, and the feasibility of design schemes is sensitive to the weight of structure. Sandwich box beam composed of carbon fib…
View article: Transition Flight Control and Simulation of a Novel Tail-Sitter UAV With Varying Fuselage Shape
Transition Flight Control and Simulation of a Novel Tail-Sitter UAV With Varying Fuselage Shape Open
This article studies the model, control and simulation on transition flight of a novel tail-sitter with vertical takeoff and landing capability. The proposed tail-sitter adopts an innovative varying fuselage shape design to break the techn…
View article: Comprehensive sizing and optimization method for series-hybrid unmanned convertiplane
Comprehensive sizing and optimization method for series-hybrid unmanned convertiplane Open
This paper presents a novel sizing and optimization approach for the emerging series-hybrid unmanned convertiplane, which can be used to translate the top-level design requirements into the design parameters corresponding to the optimal po…
View article: Comprehensive Optimization of the Unmanned Tilt-Wing Cargo Aircraft With Distributed Propulsors
Comprehensive Optimization of the Unmanned Tilt-Wing Cargo Aircraft With Distributed Propulsors Open
The unmanned tilt-wing cargo aircraft using distributed propulsors is an emerging aircraft significantly different from traditional types. This paper proposes an aerodynamic, propulsion, noise, weight integrated optimization design method …