Thermal Stress Analysis of Composite Beams, Plates and Shells

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Details

Thermal Stress Analysis of Composite Beams, Plates and Shells: Computational Modelling and Applications presents classic and advanced thermal stress topics in a cutting-edge review of this critical area, tackling subjects that have little coverage in existing resources. It includes discussions of complex problems, such as multi-layered cases using modern advanced computational and vibrational methods.

Authors Carrera and Fazzolari begin with a review of the fundamentals of thermoelasticity and thermal stress analysis relating to advanced structures and the basic mechanics of beams, plates, and shells, making the book a self-contained reference. More challenging topics are then addressed, including anisotropic thermal stress structures, static and dynamic responses of coupled and uncoupled thermoelastic problems, thermal buckling, and post-buckling behavior of thermally loaded structures, and thermal effects on panel flutter phenomena, amongst others.


Autorentext

Erasmo Carrera is a leading expert on advanced structural models for thermal stress analysis. He has published more than 30 articles on thermal stress problems, is an editorial board member for Journal of Thermal Stresses and editor-in-chief of the International Journal of Advances on Aircraft and Spacecraft Sciences


Inhalt

  1. Introduction2. Solution of sample problems in classical thermoelasticity3. Thermoelasticity, coupled and uncoupled variational formulations4. Fundamental mechanics of beams, plates and shells 5. Multilayered, anisotropic thermal stress structures6. Advanced theories for multilayered beams, plates and shells7. Through-the-thickness thermal fields in one-layer and multilayered structures8. Computational methods for thermal stress analysis9. Static response of uncoupled thermoelastic problems 10. Dynamic response of uncoupled thermoelastic problems11. Static and dynamic responses of coupled thermoelastic problems12. Thermal buckling13. Post buckling behavior of thermally loaded structures14. Thermal effect on flutter of panels15. Thermal stresses in functionally graded materials

Weitere Informationen

  • Allgemeine Informationen
    • GTIN 09780128498927
    • Genre Physics
    • Herausgeber ACADEMIC PRESS
    • Größe H229mm x B152mm x T44mm
    • Jahr 2016
    • EAN 9780128498927
    • Format Kartonierter Einband
    • ISBN 978-0-12-849892-7
    • Veröffentlichung 01.12.2016
    • Titel Thermal Stress Analysis of Composite Beams, Plates and Shells
    • Autor Carrera Erasmo , Fazzolari Fiorenzo A.
    • Untertitel Computational Modelling and Applications
    • Gewicht 700g
    • Sprache Englisch

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