Aeroelastic responses of airfoil under dynamic stall forced to oscillate by cyclic pitch input
Sign Up to like & getrecommendations! Published in 2020 at "Journal of Sound and Vibration"
DOI: 10.1016/j.jsv.2020.115366
Abstract: Abstract The helicopter blades are involved in a nonlinear aeroelastic system in which unsteady dynamic stall flow and flexible structure are coupled. This problem can be reduced to a 2D aeroelastic problem in which airfoil… read more here.
Keywords: aeroelastic responses; system; frequency; dynamic stall ... See more keywords