The Calculation of the Natural Frequency of a Cantilever Monoplane Wing

Abstract

The purpose of this report is to present a practical application of the calculation of the natural frequency of a stressed skin monoplane wing in bending and in torsion.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1930
Accession Number
ADA351999

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airfoils
  • Airplanes
  • Center Of Gravity
  • Computations
  • Coverings
  • Deflection
  • Equations
  • Frequency
  • Inertia
  • Materials
  • Modulus Of Elasticity
  • Moment Of Inertia
  • Propeller Blades
  • Resonant Frequency
  • Spars
  • Vibration

Fields of Study

  • Physics