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Book The Effect of Initial Imperfections on Optimal Stiffened Cylinders Under Torsion

Download or read book The Effect of Initial Imperfections on Optimal Stiffened Cylinders Under Torsion written by George J. Simitses and published by . This book was released on 1978 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report deals with the optimization of imperfect stiffened cylinders under destabilizing loads. The developed methodology is demonstrated through numerous examples.

Book The Effect of Initial Imperfections on Optimal Stiffened Cylinders Under Axial Compression

Download or read book The Effect of Initial Imperfections on Optimal Stiffened Cylinders Under Axial Compression written by George J. Simitses and published by . This book was released on 1977 with total page 115 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report deals with the effect of initial imperfections on optimal stiffened cylinders under axial compression. A nonlinear stability methodology is developed for analyzing such system in the presence of small initial imperfections. This methodology is then employed to assess the effectiveness of stiffened cylinders optimized on the basis of linear stability analysis.

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 1048 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1987 with total page 1126 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Critical Stress of Ring stiffened Cylinders in Torsion

Download or read book Critical Stress of Ring stiffened Cylinders in Torsion written by Manuel Stein and published by . This book was released on 1949 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A nondimensional chart is presented for the theoretical critical stress in torsion of simply supported cylinders stiffened by identical, equally spaced, torsionally weak rings. The results are obtained by solving the equation of equilibrium by means of the Galerkin method. Comparison of the theoretical results wit hthe experimental results indicates that ring-stiffened cylinders buckle on the average, at a buckling stress about 15 percent below the theoretical buckling stress presented.

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Collection of Technical Papers

Download or read book A Collection of Technical Papers written by and published by . This book was released on 1993 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The 34th AIAA ASME ASCE AHS ASC Structures  Structural Dynamics and Materials Conference  Adaptive Structures Forum  93 1520   93 1587

Download or read book The 34th AIAA ASME ASCE AHS ASC Structures Structural Dynamics and Materials Conference Adaptive Structures Forum 93 1520 93 1587 written by and published by . This book was released on 1993 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Influence of Imperfections and Edge Restraint on the Buckling of Axially Compressed Cylinders

Download or read book Influence of Imperfections and Edge Restraint on the Buckling of Axially Compressed Cylinders written by Bo O. Almroth and published by . This book was released on 1966 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recent investigations on the influence of edge conditions on the critical axial load of cylindrical shells are extended here to include cylinders with elastic edge restraint. It is shown that weak edge conditions are unlikely to affect the critical load significantly in experiments or in practice. Also the effects of symmetric initial imperfections were investigated. The critical load for cylinders with initial imperfections in the form of a cosine function was found to be somewhat lower than was indicated in a previous analysis by Koiter. The analysis also disclosed that very short cylinders would not be sensitive to the types of imperfections which were considered. A few tests were performed and their results tend to support this conclusion.

Book The Effect of Internal Pressure on the Initial Buckling of Thin walled Circular Cylinders Under Torsion

Download or read book The Effect of Internal Pressure on the Initial Buckling of Thin walled Circular Cylinders Under Torsion written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1951 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Effect of Internal Pressure on the Initial Buckling of Thin walled Circular Cylinders Under Torsion

Download or read book The Effect of Internal Pressure on the Initial Buckling of Thin walled Circular Cylinders Under Torsion written by Aeronautical Research Council and published by . This book was released on 1951 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Modern Problems of Structural Stability

Download or read book Modern Problems of Structural Stability written by Alexander P. Seyranian and published by Springer. This book was released on 2014-05-04 with total page 398 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stability of structures is one of the most important and interesting fields in mechanics. This book is dedicated to fundamental concepts, problems and methods of structural stability along with qualitative understanding of instability phenomena. The methods presented are constructive and easy to implement in computer programs. Recent exciting experiments on dynamic stability of non-conservative systems are described and shown by many photographs.

Book Journal of Applied Mechanics

Download or read book Journal of Applied Mechanics written by and published by . This book was released on 1983 with total page 726 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Buckling of Stiffened Cylinders in Axial Compression and Bending

Download or read book Buckling of Stiffened Cylinders in Axial Compression and Bending written by James P. Peterson and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Buckling data review for stiffened cylinder failures during axial compression and bending.

Book Computerized buckling analysis of shells

Download or read book Computerized buckling analysis of shells written by D. Bushnell and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 439 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways.