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Hub Loads Reduction by Modification of Blade Torsional Response



Hub Loads Reduction by Modification of Blade Torsional Response

  • Presented at Forum 39
  • 7 pages
  • SKU # : 39_0_018

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Hub Loads Reduction by Modification of Blade Torsional Response

Authors / Details: S.B.R. Kottapalli, Sikorsky Aircraft Division, UTC