The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges /

A theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges.

Bibliographic Details
Call Number:Libro Electrónico
Main Author: Seide, Paul (Author)
Corporate Authors: Langley Aeronautical Laboratory, United States. National Advisory Committee for Aeronautics
Format: Government Document Electronic eBook
Language:Inglés
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2679.
Subjects:
Plates (Engineering)
Sandwich construction.
Loads (Mechanics)
Buckling (Mechanics)
Elasticity.
Plaques (Ingénierie)
Construction sandwich.
Charges.
Flambage (Résistance des matériaux)
Élasticité.
warping.
buckling.
elasticity.
modulus of elasticity.
Elasticity
Sandwich construction
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