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Hub Vibratory Loads Reductions using Individual Blade Pitch Controls for Lift-offset Helicopter Rotors

Hub Vibratory Loads Reductions using Individual Blade Pitch Controls for Lift-offset Helicopter Rotors

  • 12 pages
  • SKU # : sm_arf_2018_dynamics_004

  • Your Price : $30.00

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Hub Vibratory Loads Reductions using Individual Blade Pitch Controls for Lift-offset Helicopter Rotors

Authors / Details: Jae-Sang Park, Chungnam National University; Do-Hyung Kim, Sang-Hyun Chae, Korea Aerospace Research Institute; Ye-Lin Lee, Chungnam National University; Jeong-In Go, Agency for Defense Development