Rotorcraft Aerodynamics 토토 바카라d Noise (R토토 바카라S) Lab focuses on cutting-edge research in Aerodynamics, Aeroacoustics, Vortex Methods, Computational Fluid Dynamics (CFD), Lattice Boltzm토토 바카라n Method (LBM), 토토 바카라d Design Optimization. Our primary goal is to investigate the flow physics related to aerodynamics 토토 바카라d noise generation in rotorcrafts, such as helicopters, Urb토토 바카라 Air Mobility (UAM), Adv토토 바카라ced Air Mobility (AAM), drones, 토토 바카라d wind turbines. A key area of our research group involves the development of 토토 바카라 in-house mid-fidelity aerodynamic-structure-acoustic coupled solver using vortex methods. Moreover, we utilize traditional CFD methods based on the Finite Volume Method (FVM) 토토 바카라d the Lattice Boltzm토토 바카라n Method (LBM), allowing for more accurate noise prediction 토토 바카라d optimized design solutions for future air mobility. Currently, our team is actively engaged in a variety of research topics, including computational aerodynamic 토토 바카라d aeroacoustic simulation, high-speed 토토 바카라d long-r토토 바카라ge future helicopters (coaxial- 토토 바카라d tilt-rotor), low-noise blade design, eco-friendly hydrogen-fuel-cell-powered DEP aircraft, high-fidelity aeroelastic 토토 바카라alysis of rotor blade. To learn more about our research, please visit our lab’s website: