Affiliation:
1. Gwangju Institute of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. High-Fidelity Computational Aerodynamics of Multi-Rotor Unmanned Aerial Vehicles
2. Rotor interactional effects on aerodynamic and noise characteristics of a small multirotor unmanned aerial vehicle
3. Effects of Rotor-Rotor Interaction on the Wake Structure and Thrust Generation of a Quadrotor Unmanned Aerial Vehicle
4. Leishman, J. G., Principles of Helicopter Aerodynamics, 3rded.Cambridge University Press, 2006, Chap. 5.7 Vortex Ring State (VRS), pp.252-257.
5. Brown, R. E. "Are eVTOL aircraft inherently more susceptible to the vortex ring state than conventional helicopter?" Sophrodyne Aerospace Technical Report, Sophrodyne Aerospace, Glasgow, United Kingdom, 2022.