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General buckling of torqued, longitudinally stiffened, 180-degree cylindrical shell specimen

FROM:

Tomasz Kopecki (Rzeszów University of Technology, Faculty of Mechanical Engineering and Aeronautics, Rzeszów, Poland), “Chapter 23: Coupling Experiment and Nonlinear Numerical Analysis in the Study of Post-Buckling Response of Thin-Walled Airframe Structures”, in the book, “Numerical Analysis – Theory and Application”, edited by Jan Awrejcewicz, ISBN 978-953-307-389-7, September 2011,
DOI: 10.5772/23226

PARTIAL INTRODUCTION: Rational approach to design of load-carrying structures seems to suggest the necessity of focusing special attention on crucial areas of these structures, which are decisive for durability and reliability of the structure. The presence of such crucial areas in a designed solution, resulting usually from its practical functions, should be given careful consideration in view of opportunity to introduce appropriate changes in the design solutions possibly before costly and time-consuming workshop realization of a prototype.
The intent of the author is to draw attention to gravity of the factor integrating nonlinear numerical analysis with an experiment – in a broad sense of this word. Then, this chapter presents a methodology that can be used for assessment and current improvement of numerical models thus ensuring correct interpretation of results obtained from nonlinear numerical analyses of a structure. The proposed methodology is based on carrying out experimental examination of selected crucial elements of load-carrying structures parallel with their nonlinear numerical analysis. Special attention is paid to factors determining proper realization of adequate experiments with emphasis placed on the role…

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