BUCKLING COEFFICIENTS FOR SIMPLY SUPPORTED, FLAT, RECTANGULAR SANDWICH PANELS UNDER BIAXIAL COMPRESSION.

Abstract

The report presents the derivation of formulas for the buckling coefficients of simply supported, flat, rectangular sandwich panels under edgewise (in-plane) biaxial compression loads. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1970
Accession Number
AD0708954

Entities

Organizations

  • Forest Products Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Buckling
  • Coefficients
  • Compression
  • Failure (Mechanics)
  • Sandwich Panels

Fields of Study

  • Physics

Readers

  • Structural Dynamics.