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Titlebook: Computerized buckling analysis of shells; D. Bushnell Book 1989 Kluwer Academic Publishers 1989 calculus.design.linearity.model.modeling.n

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書目名稱Computerized buckling analysis of shells
編輯D. Bushnell
視頻videohttp://file.papertrans.cn/235/234584/234584.mp4
叢書名稱Mechanics of Elastic Stability
圖書封面Titlebook: Computerized buckling analysis of shells;  D. Bushnell Book 1989 Kluwer Academic Publishers 1989 calculus.design.linearity.model.modeling.n
描述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 gene
出版日期Book 1989
關(guān)鍵詞calculus; design; linearity; model; modeling; numerical methods; optimization; simulation; stability
版次1
doihttps://doi.org/10.1007/978-94-009-5063-4
isbn_softcover978-94-010-8741-4
isbn_ebook978-94-009-5063-4Series ISSN 0924-2112
issn_series 0924-2112
copyrightKluwer Academic Publishers 1989
The information of publication is updating

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Mechanics of Elastic Stabilityhttp://image.papertrans.cn/c/image/234584.jpg
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Computerized buckling analysis of shells978-94-009-5063-4Series ISSN 0924-2112
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https://doi.org/10.1007/978-94-009-5063-4calculus; design; linearity; model; modeling; numerical methods; optimization; simulation; stability
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978-94-010-8741-4Kluwer Academic Publishers 1989
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The European Union in International Affairsjunk (Fig. 1). Occasionally unaware of the possibility of buckling, engineers have designed structures (Fig. 2(a)) with inadequate safety margins (Fig. 2(b)). The large cylindrical tower on the left in Fig. 3(a) failed in 1956 [1] because of buckling of a torispherical end closure at its lower end.
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https://doi.org/10.1007/978-94-009-3277-7onlinear collapse (“snap-through”) or to bifurcation buckling. The purpose of this section is to present many examples in which the failure mode is nonlinear collapse. Examples are given of axisymmetric collapse of elastic-plastic-creeping monocoque cylinders under axial compression and ring-stiffen
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