The Shearing Rigidity of Curved Panels Under Compression

Abstract

Determinations were made under comparison, particularly in that region of loading where the panels are in a buckled state. Cylinders were built and reinforced with a number of stringers and rings. Tests were made by measuring the twist angle of the cylinder caused by known amount of torque while the cylinder was subject to uniform axial compression. Shearing rigidity of a panel decreases when increasing amounts of compressive loads are applied to the panel in the axial direction.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1946
Accession Number
ADB225589

Entities

People

  • Bruno A. Boley
  • N. J. Hoff

Organizations

  • New York University Tandon School of Engineering

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aeronautical Laboratories
  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Buckling
  • Compression
  • Coverings
  • Diameters
  • Equations
  • Instability
  • Materials
  • Measurement
  • Modulus Of Elasticity
  • Moment Of Inertia
  • Shear Modulus
  • Strain Gages

Readers

  • Structural Dynamics.