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

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Bibliographic Details
Main Author Stein, Manuel
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Mayers, J.
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 2601.
Subjects
Plates (Engineering) > Curvature.
Cylinders.
Sandwich construction.
Buckling (Mechanics)
Loads (Mechanics)
Strains and stresses.
elektronické knihy
electronic books
Online AccessFull text
ISBN9781680156232
1680156233
Physical Description1 online resource (34 pages) : illustrations

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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 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
Physical Description:1 online resource (34 pages) : illustrations

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