Handbook of structural stability. Part 5, Compressive strength of flat stiffened panels /

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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. 3785.
Subjects
Online AccessFull text
ISBN9781680156300
1680156306
Physical Description1 online resource (ii, 89 pages) : illustrations

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Abstract: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.
Item Description:NACA TN No. 3785.
Bibliography:Includes bibliographical references.
ISBN:9781680156300
1680156306
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 (ii, 89 pages) : illustrations