PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Delamination resistance of laminate made with VBO MTM46/HTS prepreg

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
A laminate made with the Vacuum Bag Only (VBO) prepregs can be cured out of autoclave. Because of low curing pressure such a process can result in deterioration of laminate mechanical properties. They can be significantly lower than those displayed by the autoclave cured ones. The resistance against delamination can be among the most affected. Since this property is a week point of all the laminates it was of particular interest. Delamination resistance of unidirectional laminate made from VBO MTM46/HTS(12K) prepreg was in the scope of the presented research and the critical values of the Strain Energy Release Rates and the Paris-type equations corresponding to Mode I, Mode II and Mixed-Mode I/II static and cyclic loadings, respectively, were determined.
Słowa kluczowe
Rocznik
Strony
173--177
Opis fizyczny
Bibliogr. 15 poz., rys., tab., wykr.
Twórcy
autor
  • Institute of Aeronautics and Applied Mechanics, Warsaw University of Technology, Nowowiejska 24, 00-665 Warsaw, Poland
  • Institute of Aviation, Aleja Krakowska 110/114, 02-256 Warsaw, Poland
Bibliografia
  • 1. ASTM D5528-12 Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites
  • 2. ASTM D6115-97 Standard Test Method for Mode I Fatigue Delamination Growth Onset of Unidirectional Fiber-Reinforced Polymer Matrix Composites
  • 3. ASTM D6671-13 Standard Test Method for Mixed Mode I-Mode II Interlaminar Fracture Toughness of Unidirectional Fiber Reinforced Polymer Matrix Composites
  • 4. Bai J. (ed.) (2013), Advanced fibre–reinforced polymer (FRP) compositesfor structural application, Woodhead Pu. Ltd.
  • 5. Becht G. J., Gillespie J. W. (1989), Numerical and Experimantal Evaluation of the Mode III Interlaminar Fracture Toughness of Composite Materials, Polymer Composites, 10, 293-303.
  • 6. Czabaj M. W., Ratcliffe J. (2012), Comparison of Intralaminar and Interlaminar Mode-I Fracture Toughness of Unidirectional IM7/8552 Graphite/Epoxy Composite, NACA raport NF 16762-15094.
  • 7. Czajkowska K., Czarnocki P, Lorenc Z. (2014), Interlaminar Mode II Toughness of Unidirectional CF-Epoxy Laminates Made of out of Autoclave Prepregs, Key Engineering Materials, 598, 45-50.
  • 8. Hiley M. (2000), Delamination between multi-directional ply interfaces in carbon-epoxy composite under static and fatigue loadings, Fracture of Polymers, Composites and Adhesives, ESIS Publication 27, 41-72.
  • 9. Kim R. Y. (2001), Polymer matrix composite (PMC) damage tolerance and repair technology, Report No. UDR-TR-2001-00041.
  • 10. Lander J. K., Kawashita L. F, Allegri G, Hallett S. R, Wisnom M. R., (2010), A cut ply specimen for the determination of mixedmode interlaminar fracture toughness, 14th European Conference on Composite Materials, 1-11.
  • 11. Meziere Y., Michel L. (2000), Mixed-Mode delamination Failure criteria in Carbon Fibre/Composite under Quasi-Static and Cyclic Loadings, Fracture of Polymers, Composites and Adhesives, ESIS Publication 27, 97-110.
  • 12. Murri B., (2011), Effect of Data Reduction and Fiber-Bridging on Mode I Delamination Characterization of Unidirectional Composites, Proceedings of the American Society for Composites 26th Annual Technical Conference/2nd Joint US-Canada Conference on Composites.
  • 13. Paris I., Minguet P. J., O’Brien T. K. (2003), Comparison of Delamination Characterisation for IM7/8552 Composite Woven and Tape Laminates, ASTM STP 1436, 372-390.
  • 14. Stelzer S., Jones R., Brunner A. J. (2013), Interlaminar Fatigue Crack Growth In Carbon Fiber Reinforced Composites, The19th International Conference On Composite Materials, 1-9.
  • 15. Szekrenyes A. (2010), Crack Stability of Fractuer Specimens Used to Test Unidirectional Fiber Reinforced Material, Experimental chanics, 50, 473-482.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-b5e99270-1fad-44b6-a4cb-b9baef2d352d
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.