Buckling of Rectangular Sandwich Plates Subjected to Edgewise Compression with Loaded Edges Simply Supported and Unloaded Edges Clamped
Auteur : Kuo Tai Yen, V. L. Salerno, Nicholas John Hoff
Date de publication : 1952
Éditeur : National Advisory Committee for Aeronautics
Nombre de pages : 66
Résumé du livre
The compressive stress for buckling is calculated for a rectangular flat sandwich plate with loaded edges simply supported and unloaded edges rigidly clamped. in the calculations Hoff's differential equations are integrated by Legget's method to obtain lower bounds and by Galerkin's method to establish upper bounds. True values of the buckling stress are estimated as arithmetic means of these bounds and are presented in a diagram which covers the entire practical range of the geometric and mechanical quantities involved.