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Structural Optimization for Vibration Reduction of Composite Helicopter Rotor Blades with Advanced Geometry Tips Subject to Multidisciplinary Constraints

Structural Optimization for Vibration Reduction of Composite Helicopter Rotor Blades with Advanced Geometry Tips Subject to Multidisciplinary Constraints

  • Presented at Forum 51
  • 20 pages
  • SKU # : 51_2_004

  • Your Price : $30.00

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Structural Optimization for Vibration Reduction of Composite Helicopter Rotor Blades with Advanced Geometry Tips Subject to Multidisciplinary Constraints

Authors / Details: Kuo-An Yuan, McDonnell Douglas Corporation; Peretz P. Friedmann, University of California, Los Angeles