Author: Dalip Singh ChehilPublisher:
ISBN:
Category : Buckling
Languages : en
Pages : 166
Book Description
Elastic Buckling of Anisotropic Circular Cylinders Under Axial Compression and Torsion
Author: Dalip Singh ChehilPublisher:
ISBN:
Category : Buckling
Languages : en
Pages : 166
Book Description
Buckling of Laminated Anisotropic Imperfect Circular Cylinders Under Axial Compression
Author: Roderick Clarence TennysonPublisher:
ISBN:
Category :
Languages : en
Pages : 9
Book Description
Buckling of Thin-walled Circular Cylinders
Author: J. P. PetersonBuckling of Anisotropic Cylinders Under Axial Compression, Lateral Pressure and Torsion
Author: Raymond HoHandbook of Structural Stability
Author: George GerardPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28
Book Description
Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2
Author: Josef SingerPublisher: John Wiley & Sons
ISBN: 0471974501
Category : Technology & Engineering
Languages : en
Pages : 1140
Book Description
* Edited by Josef Singer, the world's foremost authority on structural buckling. * Time-saving and cost-effective design data for all structural, mechanical, and aerospace engineering researchers.
Computerized buckling analysis of shells
Author: D. BushnellPublisher: Springer Science & Business Media
ISBN: 9789024730995
Category : Science
Languages : en
Pages : 456
Book Description
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.
The Buckling Strength of Filament-wound Cylinders Under Axial Compression
Author: J. TasiPublisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 76
Book Description
Buckling Analysis of Laminated Anisotropic Cylinders Under Combined Loading
Author: Brian A. KosmalPublisher:
ISBN:
Category : Anisotropy
Languages : en
Pages : 79
Book Description
A linear shell theory, in general laminate form, describing the buckling behavior of thin-walled laminated anisotropic circular cylinders under combined loading is derived from elasticity theory. The theory incorporates the well-known Donnell's approximations. The theory is then applied to cylinders fabricated of plys with fibers oriented at angles of zero degrees and 90 degrees with respect to the cylinder axis. The loading scheme considered is that of combined internal (or external) pressure and axial tension (or compression). Fourier series solutions are assumed and the boundary condition of clamped ends is incorporated using principles of Fourier analysis. (Author).
The Behavior of Thin Walled Structures: Beams, Plates, and Shells
Author: Jack R. VinsonPublisher: Springer Science & Business Media
ISBN: 9400927746
Category : Science
Languages : en
Pages : 194
Book Description
This book is intended primarily as a teaching text, as well as a reference for individual study in the behavior of thin walled structural components. Such structures are widely used in the engineering profession for spacecraft, missiles, aircraft, land-based vehicles, ground structures, ocean craft, underwater vessels and structures, pressure vessels, piping, chemical processing equipment, modern housing, etc. It presupposes that the reader has already completed one basic course in the mechanics or strength of materials. It can be used for both undergraduate and graduate courses. Since beams (columns, rods), plates and shells comprise components of so many of these modern structures, it is necessary for engineers to have a working knowledge of their behavior when these structures are subjected to static, dynamic (vibration and shock) and environmental loads. Since this text is intended for both teaching and self-study, it stresses fundamental behavior and techniques of solution. It is not an encyclopedia of all research or design data, but provides the reader the wherewithal to read and study the voluminous literature. Chapter 1 introduces the three-dimensional equations oflinear elasticity, deriving them to the extent necessary to treat the following material. Chapter 2 presents, in a concise way, the basic assumptions and derives the governing equations for classical Bernoulli-Euler beams and plates in a manner that is clearly understood.