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Further Examination of the Vibratory Loads Reduction Results from the NASA/ARMY/MIT Active Twist Rotor Test

Further Examination of the Vibratory Loads Reduction Results from the NASA/ARMY/MIT Active Twist Rotor Test

  • Presented at Forum 58
  • 15 pages
  • SKU # : 58-2002-00077

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Further Examination of the Vibratory Loads Reduction Results from the NASA/ARMY/MIT Active Twist Rotor Test

Authors / Details: Wilbur, Matthew L.; Yeager, William T. Jr.; Sekula, Martin K.