Vortex ring state as a cause of a single-rotor helicopter unanticipated yaw-Reference-Cited by-同舟云学术

Vortex ring state as a cause of a single-rotor helicopter unanticipated yaw

Published:2022-01-10 Issue:3 Volume:5 Page:413-418
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Efimov Vadim V.,Chernigin Konstantin O.^ORCID

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-021-00128-4.pdf

Reference23 articles.

1. National Transportation Safety Board (2017) Loss of Tail Rotor Effectiveness in Helicopters. Safety Alert SA-062, March

2. U.S. Department of Transportation, Federal Aviation Administration, Flight Standards Service (2019) Helicopter Flying Handbook, Chapter 11, FAA-H-8083–21B: Helicopter Emergencies and Hazards, pp 18–21

3. RAAF Aircraft Research and Development Unit (1981) Bell 206B-1 Directional Control in Low Airspeed Flight, ARDU-TI-721, May

4. U.S. Department of Transportation, Federal Aviation Administration (1995) Unanticipated Right Yaw in Helicopters. Advisory Circular AC 90–95, December

5. Animitsa VA, Leont’yev VA (2011) About the “spontaneous” rotation of single-rotor helicopters. Civ Aviation High Technol 172:96–102

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