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 Author: 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:
ISBN: 9781680156232
1680156233
Physical Description: 1 online resource (34 pages) : illustrations

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Summary: 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 No. 2601.
Bibliography: Includes bibliographical references.
ISBN: 9781680156232
1680156233
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty