Author: Josef Singer
Publisher: 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.
Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2
Author: Josef Singer
Publisher: 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.
Publisher: 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.
Nonlinear Behaviour and Stability of Thin-Walled Shells
Author: Natalia I. Obodan
Publisher: Springer Science & Business Media
ISBN: 9400763654
Category : Science
Languages : en
Pages : 182
Book Description
This book focuses on the nonlinear behaviour of thin-wall shells (single- and multilayered with delamination areas) under various uniform and non-uniform loadings. The dependence of critical (buckling) load upon load variability is revealed to be highly non-monotonous, showing minima when load variability is close to the eigenmode variabilities of solution branching points of the respective nonlinear boundary problem. A novel numerical approach is employed to analyze branching points and to build primary, secondary, and tertiary bifurcation paths of the nonlinear boundary problem for the case of uniform loading. The load levels of singular points belonging to the paths are considered to be critical load estimates for the case of non-uniform loadings.
Publisher: Springer Science & Business Media
ISBN: 9400763654
Category : Science
Languages : en
Pages : 182
Book Description
This book focuses on the nonlinear behaviour of thin-wall shells (single- and multilayered with delamination areas) under various uniform and non-uniform loadings. The dependence of critical (buckling) load upon load variability is revealed to be highly non-monotonous, showing minima when load variability is close to the eigenmode variabilities of solution branching points of the respective nonlinear boundary problem. A novel numerical approach is employed to analyze branching points and to build primary, secondary, and tertiary bifurcation paths of the nonlinear boundary problem for the case of uniform loading. The load levels of singular points belonging to the paths are considered to be critical load estimates for the case of non-uniform loadings.
Analysis and Design of Marine Structures
Author: Carlos Guedes Soares
Publisher: CRC Press
ISBN: 0203874986
Category : Technology & Engineering
Languages : en
Pages : 578
Book Description
'Analysis and Design of Marine Structures' explores recent developments in methods and modelling procedures for structural assessment of marine structures:- Methods and tools for establishing loads and load effects;- Methods and tools for strength assessment;- Materials and fabrication of structures;- Methods and tools for structural design and opt
Publisher: CRC Press
ISBN: 0203874986
Category : Technology & Engineering
Languages : en
Pages : 578
Book Description
'Analysis and Design of Marine Structures' explores recent developments in methods and modelling procedures for structural assessment of marine structures:- Methods and tools for establishing loads and load effects;- Methods and tools for strength assessment;- Materials and fabrication of structures;- Methods and tools for structural design and opt
Scientific and Technical Aerospace Reports
Theory of Flexible Shells
Author: E.L. Axelrad
Publisher: Elsevier
ISBN: 0080984622
Category : Science
Languages : en
Pages : 416
Book Description
Theory of Flexible Shells
Publisher: Elsevier
ISBN: 0080984622
Category : Science
Languages : en
Pages : 416
Book Description
Theory of Flexible Shells
Computerized Buckling Analysis of Shells
Author: David Bushnell
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 810
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 810
Book Description
Advances in Applied Mechanics
Author:
Publisher: Academic Press
ISBN: 0080563929
Category : Technology & Engineering
Languages : en
Pages : 369
Book Description
Advances in Applied Mechanics
Publisher: Academic Press
ISBN: 0080563929
Category : Technology & Engineering
Languages : en
Pages : 369
Book Description
Advances in Applied Mechanics
Computerized buckling analysis of shells
Author: D. Bushnell
Publisher: Springer Science & Business Media
ISBN: 9400950632
Category : Science
Languages : en
Pages : 439
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.
Publisher: Springer Science & Business Media
ISBN: 9400950632
Category : Science
Languages : en
Pages : 439
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.
Applied Mechanics Reviews
Structural Analysis of Shells
Author: E. H. Baker
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 376
Book Description
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 376
Book Description