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http://yadda.icm.edu.pl:443/baztech/element/bwmeta1.element.baztech-article-BUJ5-0030-0062

Czasopismo

Journal of KONES

Tytuł artykułu

Finite numerical analysis of composite structure under complex loading conditions - optimal ply design of laminate

Autorzy Dębski, H. 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
Abstrakty
EN The paper presents FEA numerical analysis of composite structure subjected to complex loading conditions (tension and shear). The layered structures were characterized from the standpoint of optimal selection and strength parameters. The subject of the examinations was a composite: glass fibres reinforcedpolymers-M12/26%/TVR380R-glass prepreg system (Hexcel, R-glass fibres-undirectional, M12 epoxy resin). The composite system is use in helicopter blades. It exhibits good fatigue life and hot/wet performances up to 100° C. The strength properties were investigated according to ISO and ASTM standards. The composites for the study were pro duce d by autoclave technique. The Layup-Ply method with ABAQUS/Standard program was applied as an analysis tool which was carried out the leading of calculation. It was used an incremental iterative Newton-Raphson's method in a range of nonlinear geometric. Numerical calculation was made as a part of introduction to failure analysis composite materials. The risk of laminate's damage could be estimated as a possible appearing in dangerous points of construction. There were taken four criteria: the Maximum Stress Criterion, Tsai-Hill's Criterion, tensor criterion of Tsai-Wu and Azzi-Tsai-HiU's criterion.
Słowa kluczowe
EN finite element method   laminates   strength of composite structures   composites damage   composites optimization  
Wydawca Institute of Aviation
Czasopismo Journal of KONES
Rocznik 2010
Tom Vol. 17, No. 1
Strony 111--115
Opis fizyczny Bibliogr. 12 poz., rys.
Twórcy
autor Dębski, H.
  • Lublin University of Technology, Department of Machine Design Nadbystrzycka Street 36, 20-618 Lublin tel.:+48 81 5384201,fax: +48 81 5384200, h.debski@pollub.pl
Bibliografia
[1] Abaqus Theory Manual, Version 5.8, Hibbit, Karlsson & Sorensen, Inc. 1998.
[2] Abaqus/Standard User’s Manual, Version 6.5, Hibbit, Karlsson & Sorensen, Inc. 2005.
[3] Alfano, G., Crisfield, M. A., Finite element interface models for the delamination Analysis of laminated composites, Mechanical and Computational Issues, International Journal for Numerical Methods in Engineering, Vol. 50, pp. 1701-1736, 2001.
[4] Aceves, C. M., Skordos, A. A., Sutcliffe, M. P. F., Design selection methodology for composite structures, Materials&Design 29, pp. 418-426, 2008.
[5] Campbell, F. C., Manufacturing Technology for Aerospace Structural Materials, Elsevier 2006.
[6] Freeman, W. T., The Use of Composites in Aircraft Primary Structure, Composites Engineering, Vol. 3, No. 7-8, pp. 767-775, 1993.
[7] Hyla, I., Śledziona, J., Kompozyty. Elementy mechaniki i projektowania, Wydawnictwo Politechniki Śląskiej, Gliwice 2004.
[8] Miracle, D. P., Donaldson, S. L. (eds), ASM Handbook, Composites, ASM International, Vol. 21, 2001.
[9] Rusiński, E., Czmochowski, J., Smolnicki, T., Zaawansowana metoda elementów skończonych w konstrukcjach nośnych, Oficyna Wydawnicza Politechniki Wrocławskiej, Wrocław 2000.
[10] Swanson, S. R., Introduction to Design and Analysis with Advanced Composite Materials, Prentice-Hall, Inc., 1997.
[11] Tenek, L. T., Argyris, J., Finite Element Analysis of Composite Structures, Kluwer, 1998.
[12] Tsai, S. W., Introduction to Composite Materials, Technomic, 1980.
Kolekcja BazTech
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