Literature Review and Mathematical Modeling on Buckling of Laminates

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Details

The material presented in this book is intended to serve as an introduction , literature review and mathematical modeling of laminated plates on buckling of composite laminated plates. In chapter one, the introduction was presented from the points of view of fundamental definitions of fibrous composite laminates and micromechanical properties of fibers and matrix materials. At the end of the chapter the objectives of the present work were cited. Chapter two contains a comprehensive literature review which includes continuous developments in the theories of laminated plates. Also, a survey of numerical techniques which could be used in the analysis of laminated plates. In chapter three mathematical formulation and numerical modeling of laminated composite plates subjected to in - plane buckling load were derived and discussed thoroughly. Chapter four contains the conclusion of the present book. In this chapter the important observations and findings were explained clearly. The book is suitable as a review on theories of plates, mathematical modeling and numerical and / or analytical techniques subjected to bending, buckling and vibration of laminated plates.

Autorentext

Osama Mohammed Elmardi Suleiman Khayal was born in Atbara, Sudan, in 1966. He received a bachelor degree in mechanical engineering from Sudan University of science and technology Faculty of engineering Khartoum, Sudan, in 1998, and a master degree in laminated composite structural materials in 2003. He works as assistant professor in NVU, Sudan.

Weitere Informationen

  • Allgemeine Informationen
    • GTIN 09786202080743
    • Genre Mechanical Engineering
    • Sprache Englisch
    • Anzahl Seiten 80
    • Herausgeber LAP LAMBERT Academic Publishing
    • Größe H220mm x B150mm x T5mm
    • Jahr 2017
    • EAN 9786202080743
    • Format Kartonierter Einband (Kt)
    • ISBN 6202080744
    • Veröffentlichung 28.11.2017
    • Titel Literature Review and Mathematical Modeling on Buckling of Laminates
    • Autor Osama Mohammed Elmardi Suleiman
    • Gewicht 137g

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