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Application of Damage Tolerance Methodology to Helicopter Dynamic Components Using the Example of a Main Rotor Pitch Link for the AH-1S Helicopter



Application of Damage Tolerance Methodology to Helicopter Dynamic Components Using the Example of a Main Rotor Pitch Link for the AH-1S Helicopter

  • Presented at Forum 44
  • 14 pages
  • SKU # : 44_0_072

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Application of Damage Tolerance Methodology to Helicopter Dynamic Components Using the Example of a Main Rotor Pitch Link for the AH-1S Helicopter

Authors / Details: B.R. Krasnowski and W.W. Spence, Bell Helicopter Textron, and K.M. Rotenberger, U.S. Army Aviation Systems Command