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Rotorcraft Airframe Structural Optimization for Combined Vibration and Fatigue Constraints



Rotorcraft Airframe Structural Optimization for Combined Vibration and Fatigue Constraints

  • Presented at Forum 47
  • 13 pages
  • SKU # : 47_2_008
  • Your Price : $30.00
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Rotorcraft Airframe Structural Optimization for Combined Vibration and Fatigue Constraints

Authors / Details: D. Schrage and A. Sareen, Georgia Institute of Technology and T.S. Murthy, Lockheed