NACA-TR-734

Critical Compressive Stress for Outstanding Flanges

Note:

This document has not been validated by ESDU. It is provided to our users as a useful reference source.

Abstract:

A chart is presented for the values of the coefficient in the formula for the critical compressive stress at which buckling may be expected to occur in outstanding flanges. These flanges are flat rectangular plates supported along the loaded edges, supported and elastically restrained along one unloaded edge, and free along the other unloaded edge. The mathematical derivations of the formulas required for construction of the chart are given.

Author(s):
E.E. Lundquist; E.Z. Stowell

Indexed under:

  • None

Details:

NACA-TR-734
Format:
  • PDF (from scanned original)
Status:
  • Original, issued 01 Jan 1942
Previous Releases:
  • None available