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Aeroelastic Stability Characteristics of a V/STOL Tilt-Rotor Aircraft with Hingeless Blades: Analysis and Test Correlation

Aeroelastic Stability Characteristics of a V/STOL Tilt-Rotor Aircraft with Hingeless Blades: Analysis and Test Correlation

  • Presented at Forum 30
  • 12 pages
  • SKU # : 30_0_022

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Aeroelastic Stability Characteristics of a V/STOL Tilt-Rotor Aircraft with Hingeless Blades: Analysis and Test Correlation

Authors / Details: H. R. Alexander and L. M. Hengen, Boeing Vertol Co. and W. J. Weiberg, NASA - Ames Res. Center. (Standby)