Calculation of the Bending Stresses in Helicopter Rotor Blades

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1951
Accession Number
ADB184518

Entities

People

  • P. De Guillenchmidt

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aircrafts
  • Airframes
  • Bending Moments
  • Bending Stress
  • Blades
  • Centrifugal Force
  • Differential Equations
  • Equations
  • Fourier Series
  • Frequency
  • Helicopter Rotors
  • Helicopters
  • Resonant Frequency
  • Rotary Wing Aircraft
  • Two Dimensional
  • Vibration