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Determination of Rotary Wing MAV Stability Derivatives in Hover Using a Forced Oscillation Test Stand

Determination of Rotary Wing MAV Stability Derivatives in Hover Using a Forced Oscillation Test Stand

  • Presented at Forum 61
  • 9 pages
  • SKU # : 61-2005-000159

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Determination of Rotary Wing MAV Stability Derivatives in Hover Using a Forced Oscillation Test Stand

Authors / Details: Everson, Daniel; Samuel, Paul; Pines, Darryll. J.