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

Bibliographic Details
Main Author: Seide, Paul
Corporate Authors: Knovel (Firm), United States. National Advisory Committee for Aeronautics
Format: Government Document eBook
Language:English
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.
Electronic books.
Online Access:Connect to the full text of this electronic book
Description
Abstract: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.
Item Description:"April 1952."
NACA TN Number 2679.
Physical Description:1 online resource (30 pages) : illustrations.
Bibliography:Includes bibliographical references.
ISBN:9781680156249
1680156241