A5090165568- Plasma and Flow Control in Aerodynamics
- Aerodynamics and Fluid Dynamics Research
- Optimization and Packing Problems
- Aerospace and Aviation Technology
- Optimization and Search Problems
- Fluid Dynamics and Turbulent Flows
- Real-time simulation and control systems
- Metaheuristic Optimization Algorithms Research
- Advanced Optimization Algorithms Research
- Computational Fluid Dynamics and Aerodynamics
- Advanced Control Systems Optimization
- Optimization and Variational Analysis
- Air Traffic Management and Optimization
University of Chinese Academy of Sciences
2023-2024
University of Leeds
2023-2024
Nanjing University of Aeronautics and Astronautics
2016
A numerical study of the dynamic performance a circulation controlled (CC) airfoil is performed to explore feasibility using control as means gust suppression. Steady and unsteady two-dimensional computational fluid dynamics (CFD) simulations were initially validated published data. The CC was subsequently assessed. response step sinusoidal inputs obtained from CFD simulations. It found that actuation speed significantly faster than conventional mechanical flap at same flight condition....
We develop a computational fluid dynamics (CFD) framework to design feedback circulation control system compensate for fluctuations in the fixed-wing aircraft caused by wind gusts. Circulation actions are realized using dynamic boundary conditions CFD simulations. The flow responses with obtained solving unsteady Reynolds-averaged Navier-Stokes equations. lift at several oscillation frequencies of gusts and plenum chamber pressure, which controls circulation, also obtained. A identification...
A miniature air data system based on a seven-hole probe was developed for real-time, in-flight measurement of wind flow deviation angle and inertial parameters. The is very small in size weighs only 150 g, especially suitable flight tests with unmanned aerial vehicles (UAVs). It capable measuring attack (AOA) sideslip (AOS), ranging up to ±78°. exposed part slender fixed the nose aircraft, which 4 mm diameter. spin test conducted delta-wing, body aircraft; experimental results demonstrate...