Accession Number:

ADB185622

Title:

Critical Combinations of Shear and Longitudinal Direct Stress for Long Plates with Transverse Curvature

Descriptive Note:

Technical note

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA

Report Date:

1947-06-01

Pagination or Media Count:

39.0

Abstract:

A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simple supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simple supported plates.

Subject Categories:

  • Aircraft
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE