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Vibration Reduction in Rotorcraft Using the Actively Controlled Trailing Edge Flap and Issues Related to Practical Implementation

Vibration Reduction in Rotorcraft Using the Actively Controlled Trailing Edge Flap and Issues Related to Practical Implementation

  • Presented at Forum 54
  • 18 pages
  • SKU # : 54-00128

  • Your Price : $30.00

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Vibration Reduction in Rotorcraft Using the Actively Controlled Trailing Edge Flap and Issues Related to Practical Implementation

Authors / Details: Timothy F. Myrtle, University of California; Peretz P. Friedmann, University of California