An edition of Handbook of structural stability (1957)

Handbook of structural stability

Failure of plates and composite elements

Handbook of structural stability
George Gerard, George Gerard
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Last edited by MARC Bot
December 19, 2022 | History
An edition of Handbook of structural stability (1957)

Handbook of structural stability

Failure of plates and composite elements

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.

Publish Date
Language
English
Pages
93

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Edition Availability
Cover of: Handbook of structural stability
Handbook of structural stability: Compressive strength of flat stiffened panels
1957, National Advisory Committee for Aeronautics
in English
Cover of: Handbook of structural stability
Handbook of structural stability: Buckling of curved plates and shells
1957, National Advisory Committee for Aeronautics
in English
Cover of: Handbook of structural stability
Handbook of structural stability: Buckling of flat plates
1957, National Advisory Committee for Aeronautics
in English
Cover of: Handbook of structural stability
Handbook of structural stability: Failure of plates and composite elements
1957, National Advisory Committee for Aeronautics
in English

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Book Details


Edition Notes

NACA TN No. 3784.

Includes bibliographical references.

Published in
Washington, D.C
Series
Technical note / National Advisory Committee for Aeronautics -- 3784, Technical note (United States. National Advisory Committee for Aeronautics) -- no. 3784.

Classifications

Dewey Decimal Class
623.817
Library of Congress
TA645

The Physical Object

Pagination
1 online resource (ii, 93 pages)
Number of pages
93

ID Numbers

Open Library
OL44477656M
ISBN 10
1680156292
ISBN 13
9781680156294
OCLC/WorldCat
914329610

Source records

marc_columbia MARC record

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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December 19, 2022 Created by MARC Bot Imported from marc_columbia MARC record