Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2 PDF Download
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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.
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.
Author: J.G. Teng Publisher: CRC Press ISBN: 1482295075 Category : Technology & Engineering Languages : en Pages : 518
Book Description
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
Author: D. Bushnell Publisher: 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.
Author: Manuel Stein Publisher: ISBN: Category : Buckling (Mechanics) Languages : en Pages : 24
Book Description
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.
Author: Josef Singer
Author: Josef Singer
Author: United States. National Advisory Committee for Aeronautics
Author: J.G. Teng
Author: D. Bushnell
Author: Manuel Stein
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: William Arthur Nash
Author: United States. National Advisory Committee for Aeronautics
Author: