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Handbook of Structural Stability. Part III. Buckling of Curved Plates and Shells

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:28:06Z
date available2017-09-04T16:28:06Z
date copyright08/01/1957
date issued1957
identifier otherUEYHUEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/91286
description abstractAvailable 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. (author)
languageEnglish
titleNACA-TN-3783num
titleHandbook of Structural Stability. Part III. Buckling of Curved Plates and Shellsen
typestandard
page160
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1957
contenttypefulltext
subject keywordsAXIAL COMPRESSION LOADS
subject keywordsBENDING
subject keywordsBUCKLING
subject keywordsCIRCULAR CYLINDERS
subject keywordsCOMPRESSIVE STRENGTH
subject keywordsCYLINDRICAL BODIES
subject keywordsDYNAMIC STRUCTURAL ANALYSIS
subject keywordsHANDBOOKS
subject keywordsLOADS (FORCES)
subject keywordsPLASTIC DEFORMATION
subject keywordsPLATES (STRUCTURAL MEMBERS)
subject keywordsSHEAR STRENGTH
subject keywordsSHELLS (STRUCTURAL FORMS)
subject keywordsSTRUCTURAL STABILITY
subject keywordsTORSION


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