Tests of 10-Inch 24S-T Aluminum-Alloy Shear Panels with 1.5-Inch Holes. 2 - Panels Having Holes with Notched Edges

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1944
Accession Number
ADA801089

Entities

People

  • L. R. Levin
  • Paul Kuhn

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Materials
  • Shear Stresses
  • Stress Analysis
  • Stress Concentration
  • Stress Strain Relations
  • Stresses