The General Instability of Eccentrically Stiffened Cylindrical Shells Under Axial Compression and Lateral Pressure PDF Download
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Author: John N. Dickson
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 124
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Book Description
Author: John N. Dickson
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 124
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Book Description
Author: John N. Dickson
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 124
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Book Description
Author: James P. Peterson
Publisher:
ISBN:
Category : Axial compression and bending
Languages : en
Pages : 36
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Book Description
Buckling data review for stiffened cylinder failures during axial compression and bending.
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 966
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 332
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 722
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Book Description
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.
Author: D. Bushnell
Publisher: Springer Science & Business Media
ISBN: 9789024730995
Category : Science
Languages : en
Pages : 456
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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: J.G. Teng
Publisher: CRC Press
ISBN: 1482295075
Category : Technology & Engineering
Languages : en
Pages : 518
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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: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2088
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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