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Modelling the Effects of Blade Torsional Flexibility in Helicopter Stability and Control



Modelling the Effects of Blade Torsional Flexibility in Helicopter Stability and Control

  • Presented at Forum 39
  • 11 pages
  • SKU # : 39_0_047
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Modelling the Effects of Blade Torsional Flexibility in Helicopter Stability and Control

Authors / Details: H.C. Curtiss Jr. & Z. Gao, Princeton University