COMBINED-STRESS FATIGUE STRENGTH OF 76S-T61 ALUMINUM ALLOY WITH SUPERIMPOSED MEAN STRESSES AND CORRECTIONS FOR YIELDING

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1953
Accession Number
AD0010717

Entities

People

  • William N. Findley

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Aluminum Alloys
  • Axial Loads
  • Bending Moments
  • Crystal Structure
  • Engineering
  • Internal Pressure
  • Materials
  • Mechanical Properties
  • Mechanics
  • Modulus Of Elasticity
  • Residual Stress
  • Shear Stresses
  • Stress Concentration
  • Stress Strain Relations
  • Stresses
  • Yield Strength