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Flight Test of an Active Vibration Control Sytem on the UH-60 Black Hawk Helicopter

Flight Test of an Active Vibration Control Sytem on the UH-60 Black Hawk Helicopter

  • Presented at Forum 51
  • 10 pages
  • SKU # : 51_1_029

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Flight Test of an Active Vibration Control Sytem on the UH-60 Black Hawk Helicopter

Authors / Details: W. Welsh and C. Fredrickson, Sikorsky Aircraft Corporation; I. Lyndon, Westland Helicopters Ltd.; C. Rauch, Moog Inc.