The Influence Of Prebuckling Deformations And Stresses On The Buckling Of Perfect Cylinders
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The Influence of Prebuckling Deformations and Stresses on the Buckling of Perfect Cylinders
Author | : Manuel Stein,United States. National Aeronautics and Space Administration |
Publsiher | : Unknown |
Total Pages | : 32 |
Release | : 1964 |
Genre | : Buckling (Mechanics) |
ISBN | : NASA:31769000422298 |
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Large-deflection theory is used to compute buckling loads of simply supported initially perfect cylinders under axial compression, external pressure, and combinations of axial compression and internal or external pressure. Important results are obtained by taking into account prebuckling deformations and stresses induced by edge support. For example, the presence of these deformations and stresses can reduce the axial-compression buckling load of an unpressurized perfect cylinder to 50 percent of the classical value.
NASA Technical Report
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 540 |
Release | : 1964 |
Genre | : Aerodynamics |
ISBN | : MINN:31951000846626X |
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The Influence of Prebuckling Deformations and Stresses on the Buckling of Perfect Cylinders
Author | : Manuel Stein |
Publsiher | : Unknown |
Total Pages | : 32 |
Release | : 1964 |
Genre | : Buckling (Mechanics) |
ISBN | : UIUC:30112106681965 |
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Buckling of Thin Metal Shells
Author | : J.G. Teng,J.M. Rotter |
Publsiher | : CRC Press |
Total Pages | : 520 |
Release | : 2006-06-28 |
Genre | : Technology & Engineering |
ISBN | : 9781482295078 |
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Thin-walled metal shell structures are highly efficient in their use of material, but they are particularly sensitive to failure by buckiling. Many different forms of buckling can occur for different geometries and different loading conditions. Because this field of knowledge is both complex and industrially important, it is of great interest and c
Elastic Stability of Circular Cylindrical Shells
Author | : N. Yamaki |
Publsiher | : Elsevier |
Total Pages | : 573 |
Release | : 1984-02-01 |
Genre | : Science |
ISBN | : 9780444599117 |
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The object of this book is to clarify the whole aspect of the basic problems concerning the elastic stability of of circular cylindrical shells under typical loading conditions. The book deals with buckling, postbuckling and initial postbuckling problems under one of the three fundamental loads, that is, torsion, pressure and compression. The emphases are placed on the accurate analysis and comprehensive numeral results for the buckling problem, experimental verification of the theoretical analysis for the postbuckling problem and clarification of the range of applicability of the perturbation method for the analysis of initial postbuckling behaviors and imperfection sensitivity. The problems under typical combined loads as well as the influence of the contained liquid are also clarified.
Stability Analysis of Plates and Shells
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 460 |
Release | : 1998 |
Genre | : Plates (Engineering) |
ISBN | : PSU:000032591033 |
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NASA Scientific and Technical Reports
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publsiher | : Unknown |
Total Pages | : 1152 |
Release | : 1965 |
Genre | : Aeronautics |
ISBN | : STANFORD:36105113793751 |
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A Selected Listing of NASA Scientific and Technical Reports for
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publsiher | : Unknown |
Total Pages | : 1156 |
Release | : 1964 |
Genre | : Aeronautics |
ISBN | : CORNELL:31924057848818 |
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