RESEARCH OF THE HIGH HARMONICS INDIVIDUAL BLADE CONTROL EFFECT ON VIBRATIONS CAUSED BY THE HELICOPTER MAIN ROTOR THRUST

Article Russian OPEN
(2017)
  • Publisher: Moscow State Technical University of Civil Aviation
  • Journal: Naučnyj Vestnik MGTU GA (issn: 2079-0619, eissn: 2542-0119)
  • Publisher copyright policies & self-archiving
  • Related identifiers: doi: 10.26467/2079-0619-2016-19-6-68-76
  • Subject: вертолет | несущий винт | индивидуальное управление лопастями | аэродинамические ха- рактеристики | виброперегрузка | вихревая теория | Motor vehicles. Aeronautics. Astronautics | TL1-4050

The paper presents numerical results analysis of main rotor vibration due to helicopter main rotor thrust pulsation.The calculation method, the object of research and numerical research results with the aim to reduce the amplitude of the vibrations transmitted to the hu... View more
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