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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.
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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. 3785.
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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