Tytuł artykułu
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Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Konferencja
12th International Scientific Conference CAM3S'2006, 27-30th November 2006, Gliwice-Zakopane
Języki publikacji
Abstrakty
Purpose: The study aims to identify elastic properties of laminated plates from the measured dynamical properties. Design/methodology/approach: Elastic constants of laminates have been determined by using an identification procedure based on experiment design, and multi-level theoretical approach. Findings: The present paper is the first attempt at proposing a novel procedure to derive stiffness parameters from forced sandwich plates. The main advantage of the present method is that it does not rely on strong assumptions on the model of the plate. The key feature is that the raw models can be applied at different vibration conditions of the plate by a suitable analytical ore approximation method. Research limitations/implications: In the future the extension of the present approach to sandwich plates will be performed in order to test various experimental conditions. Practical implications: Structures composed of laminated materials are among the most important structures used in modern engineering and especially in the aerospace industry. Such lightweight and highly reinforced structures are also being increasingly used in civil, mechanical and transportation engineering applications. Originality/value: The main advantage of the present method is that it does not rely on strong assumptions on the model of the plate. The key feature is that the raw models can be applied at different vibration conditions of the plate by a suitable analytical ore approximation method.
Wydawca
Rocznik
Tom
Strony
227--230
Opis fizyczny
Bibliogr. 10 poz., rys.
Twórcy
Bibliografia
- [1] CM. Mota Soares, M. Moreira de Freitas, AL. Arauajo, Identification of material properties of composite plate specimens. Composite Structures 1993; 25:277-285.
- [2] A.L. Araujo, CM. Mota Soares, M.J. Moreira de Freitas, P. Pedersen, J. Herskovits. Combined numerical-experimental model for the identification of mechanical properties of laminated structures Composite Structures 2000, 50:363 – 372.
- [3] R. Rikards, A. Chate, Optimal design of sandwich and laminated composite plates based on planning of experiments, International Journal of Solids and Structure 1995; 10 (l):46-53.
- [4] M.K. Rao, Y.M. Desai. Analytical solutions for vibrations of laminated and sandwich plates using mixed theory. Composite Structures 63 (2004) 361-373.
- [5] K. Jawahar Reddy and K. Vijayakumarf, Cylindrical bending of angle-ply laminates subjected to different sets of edge boundary conditions. Computer and Structure Vol. 56. No. I, pp. 147-155. 1995.
- [6] Xiao-Ping Shua, P. Kostas, B. Soldatos, Cylindrical bending of angle-ply laminates subjected to different sets of edge boundary conditions. International Journal of Solids and Structures 37 (2000) 4289-4307.
- [7] Song-Jeng Huang. An analytical method for calculating the stress and strain in adhesive layers in sandwich beams. Composite Structures 60 (2003) 105-114.
- [8] Zhuang Li, Bohdan Diveyev, Malcolm J. Crocker. Refined Numerical Schemes for a Stressed-Strained State of Layered Elements for damping estimation. Theoretical foundations. (In press).
- [9] Zhuang Li, Bohdan Diveyev, Malcolm J. Crocker. Refined Numerical Schemes for a Stressed-Strained State of Layered Elements for damping estimation. 2. Damping Bounds Predictions and Experimental Modelling (In press).
- [10] Bohdan Diveyev, Malcolm J. Crocker. Dynamic properties and damping prediction for laminated plates (In press).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BOS5-0018-0046