Handbook of structural stability. Part 3, Buckling of curved plates and shells /

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Bibliographic Details
Main Author Gerard, George
Corporate Author United States. National Advisory Committee for Aeronautics
Other Authors Becker, Herbert, 1918-
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : National Advisory Committee for Aeronautics, [1957]
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; no. 3783.
Subjects
Online AccessFull text
ISBN9781680156287
1680156284
Physical Description1 online resource (iii, 154 pages) : illustrations

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Abstract:Available theories and test data on buckling of curved plates and shells are reviewed. For torsion and external-pressure loadings, the test data are correlated in terms of linear buckling theories for both the elastic and inelastic ranges.
The cases which exhibit a marked disagreement between linear theory and test data include those of curved plates and cylinders under axial compression, cylinders under bending, and spherical plates under external pressure. These cases have been analyzed by a unified semiempirical approach for both the elastic and inelastic ranges which is satisfactory for analysis and design purposes.
The effects of internal pressure on buckling of elements under uniaxial loads are discussed and data on various combined loadings are presented in interaction form.
Item Description:NACA TN No. 3783.
Bibliography:Includes bibliographical references.
ISBN:9781680156287
1680156284
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 (iii, 154 pages) : illustrations