Open AccessA Review on Vibration Analysis of Helicopter Rotor Blade
Author(s) -
Bilji C Mathew,
Prasun Banerjee,
Muhammad Fawaz,
Samprit Roy,
Aritra Laha,
Manasa Bhatt
Publication year - 2022
Publication title -
international journal for research in applied science and engineering technology
Language(s) - English
Resource type - Journals
ISSN - 2321-9653
DOI - 10.22214/ijraset.2022.40533
Subject(s) - vibration , rotor (electric) , helicopter rotor , blade (archaeology) , engineering , structural engineering , drag , aerospace engineering , mechanical engineering , acoustics , physics
Vibration has always been a major disturbance for helicopter. Vibrations, thus, a threat to components of helicopter. The vibration created by a helicopter draws a great contribution to the reduction in life of the components. Reducing the vibration that creates from helicopter rotor blades, tail rotors is a one step closer to this crisis. Helicopter Vibration control is a topic of research into designing helicopter rotor blade which can be operated more efficiently. The major source of the vibration come from the rotor blade rotation. By trying to upgrade new design in the helicopter main rotor blades and tail rotors reduce the vibration and make the operation more efficient. This paper addresses simulation and analysis of vibration level of rotor blades. Keywords: drag, rotor, vibration, air foil, blade profile.