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Compressive buckling of simply supported curved plates and cylinders of sandwich construction /

Bibliographic Details
Main Author: Stein, Manuel
Corporate Authors: Knovel (Firm), United States. National Advisory Committee for Aeronautics
Other Authors: Mayers, J.
Format: eBook
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2601.
Subjects:
Plates (Engineering) > Curvature.
Cylinders.
Sandwich construction.
Buckling (Mechanics)
Loads (Mechanics)
Strains and stresses.
Electronic books.
Online Access:Connect to the full text of this electronic book
Description
Abstract:Theoretical solutions are presented for the buckling in uniform axial compression of two types of simply supported curved sandwich plates: the corrugated-core type and the isotropic type. Results are given in the form of equations and curves.
Item Description:"January 1952."
NACA TN Number 2601.
Electronic resource.
Physical Description:1 online resource (34 pages) : illustrations.
Bibliography:Includes bibliographical references.
ISBN:9781680156232
1680156233