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A Method for Determining the Fully Coupled Aeroelastic Response of Helicopter Rotor Blades

A Method for Determining the Fully Coupled Aeroelastic Response of Helicopter Rotor Blades

  • Presented at Forum 19
  • 10 pages
  • SKU # : 19_0_004

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A Method for Determining the Fully Coupled Aeroelastic Response of Helicopter Rotor Blades

Authors / Details: Edward R. Wood, and Kurt D. Hilzinger, Sikorsky Aircraft Div.