Early Onset Prediction for Rotors in Vortex Ring State-Reference-Cited by-同舟云学术

Early Onset Prediction for Rotors in Vortex Ring State

Published:2020-11 Issue:6 Volume:33 Page:04020081
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

McQuaid Joel¹^ORCID,Kolaei Amir²,Bramesfeld Götz³^ORCID,Walsh Paul⁴

Affiliation:

1. M.A.Sc. Candidate, Dept. of Aerospace Engineering, Faculty of Engineering and Architectural Science, Ryerson Univ., Toronto, ON, Canada M5B 2K3 (corresponding author). ORCID: .

2. Postdoctoral Fellow, Dept. of Aerospace Engineering, Faculty of Engineering and Architectural Science, Ryerson Univ., Toronto, ON, Canada M5B 2K3.

3. Associate Professor, Dept. of Aerospace Engineering, Faculty of Engineering and Architectural Science, Ryerson Univ., Toronto, ON, Canada M5B 2K3. ORCID: .

4. Professor, Dept. of Aerospace Engineering, Faculty of Engineering and Architectural Science, Ryerson Univ., Toronto, ON, Canada M5B 2K3.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001194

Reference27 articles.

1. Ahlin G. A. and R. E. Brown. 2005. “Investigating the physics of rotor vortex ring state using the vorticity transport model.” In Proc. 31st European Rotorcraft Forum 1–15. Florence Italy: Dept. of Aeronautics Imperial College.

2. Induced flow variation of the helicopter rotor operating in the vortex ring state.

3. Betzina M. D. 2001. “Tiltrotor descent aerodynamics: A small-scale experimental investigation of vortex ring state.” In Proc. American Helicopter Society 57th Annual Forum 1–12. Washington DC: NASA Ames Research Center.

4. Brand A. M. Dreier R. Kisor and T. Wood. 2007. “The nature of vortex ring state.” In Proc. American Helicopter Society 63rd Annual Forum 1–14. Virginia Beach VA: Bell Helicopter Textron Inc.

5. Brown R. E. S. J. Newman J. G. Leishman and F. J. Perry. 2002. “Blade twist effects on rotor behaviour in the vortex ring state.” In Proc. European Rotorcraft Forum 1–14. Bristol UK: Imperial College of Science Technology & Medicine.

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1. Effects of rotor separation on the axial descent performance of dual-rotor configurations;Flow;2023

2. Formation of a shockwave from subsonic vortex ring collisions of varying geometries;SHOCK COMPRESSION OF CONDENSED MATTER - 2022: Proceedings of the Conference of the American Physical Society Topical Group on Shock Compression of Condensed Matter;2023

3. Time and Energy Efficient Descent Trajectories for Quadcopters that Avoid the Vortex Ring State;2022 IEEE Conference on Control Technology and Applications (CCTA);2022-08-23