An edition of Handbook of structural stability (1957)

Handbook of structural stability

Compressive strength of flat stiffened panels

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

Compressive strength of flat stiffened panels

A generalized crippling analysis for short monolithic panels with formed or extruded stiffeners is presented. The analysis applies to monolithic panels. Criteria are given for rivete panels which indicate if the panels can be considered to behave in a monolithic manner. Riveted panels that are subject to interrivet buckling and wrinkling or forced crippling do not behave in this manner. Methods are presented for estimating the strength of such panels.

Intermediate-length and long stiffened panels are subject to other failure modes. Methods are given for estimating the column strength of panels. Various forms of column curves and direct-reading charts are considered. Theory and test data on optimum stiffened panels are presented for use in preliminary design studies.

In box types of construction, the rib and spar structures influence the compressive strength of the stiffened panel. The various factors which can be of importance are considered.

Publish Date
Language
English
Pages
89

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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. 3785.

Includes bibliographical references.

Published in
Washington, D.C
Series
Technical note / National Advisory Committee for Aeronautics -- 3785, Technical note (United States. National Advisory Committee for Aeronautics) -- no. 3785.

Classifications

Dewey Decimal Class
623.817
Library of Congress
TA645

The Physical Object

Pagination
1 online resource (ii, 89 pages)
Number of pages
89

ID Numbers

Open Library
OL44477658M
ISBN 10
1680156306
ISBN 13
9781680156300
OCLC/WorldCat
914329651

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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