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

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.

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Bibliographic Details
Main Author: Stein, Manuel
Corporate Authors: United States. National Advisory Committee for Aeronautics, Knovel (Firm)
Other Authors: Mayers, J.
Format: Electronic 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:
Online Access: Full text (Wentworth users only)