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Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavior, effective width, and failure of flat curved plates are correlated.
Test data on the crippling strength of various formed and extruded shapes are reviewed, from which a generalized method of crippling analysis is formulated. The effects upon the crippling strength of alclad coatings and the increased properties in the corners of formed sections are investigated by use of this analysis.
The generalized crippling analysis was applied to a variety of sections and materials in common use. It was found that the crippling strength of all the sections is governed in a simple manner by the developed length-thickness ratio and number of corners of the section.
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Subjects
Structural analysis (Engineering), Stability, Plates (Engineering), Curvature, Shells (Engineering), Buckling (Mechanics), Loads (Mechanics), Strains and stresses, Théorie des constructions, Stabilité, Flambage (Résistance des matériaux), Charges, Contraintes (Mécanique), Structural analysisShowing 4 featured editions. View all 4 editions?
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1
Handbook of structural stability: Compressive strength of flat stiffened panels
1957, National Advisory Committee for Aeronautics
in English
1680156306 9781680156300
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2
Handbook of structural stability: Buckling of curved plates and shells
1957, National Advisory Committee for Aeronautics
in English
1680156284 9781680156287
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3
Handbook of structural stability: Buckling of flat plates
1957, National Advisory Committee for Aeronautics
in English
1680156268 9781680156263
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4
Handbook of structural stability: Failure of plates and composite elements
1957, National Advisory Committee for Aeronautics
in English
1680156292 9781680156294
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Book Details
Edition Notes
NACA TN No. 3784.
Includes bibliographical references.
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Work Description
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.
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