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Low velocity impact damage in glass / polyester composite sandwich panels

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Impact resistance of glass/polyester facesheets/PVC foam core sandwich structures was primarily assessed in terms of skin-/core bonding efficiency using two types of adhesives and bonding with uncured resin. Also, the air-coupled ultrasonic C-scan technique was estimated as a means of characterizing impact damage size in sandwich structures. The following observations were made. The impact damage size estimated by visual inspection was much more extensive in all samples, which is due to the C-scan images showing only the overlapping delaminations area directly under the impact site, whereas the visual inspection of the laminate surface and macroscopic observations of the sample section show the extent of the largest, single delamination. The least extensive damage size was found in the two-phase high-density adhesive samples showing also the highest tendency for core cracking. In contrast, the “pinkglue” adhesive, which is low-density due to the presence of the microspheres provides greater local flexibility which prevented core craking.
Rocznik
Strony
26--34
Opis fizyczny
Bibliogr. 12 poz., rys.
Twórcy
autor
autor
autor
  • Michelin Polska, Olsztyn, Poland
Bibliografia
  • 1. Buli P.H., Edgren F., Compressive strength after impact ofCFRP-foam córę sandwich panels in marinę applicalions, Composites, Part B, 35 (2004), pp. 535-541.
  • 2. Abratc S., Impact on composite structures, Cambridge University Press, 1998.
  • 3. Wen H.M., Reddy T. Y., Reid S.R., Soden P.D., Indentation, penetration and perforation of composite laminates and sandwich panels under quasi-static and projectile loading, Key Enginering Materials, 141-143 (1998), pp. 501-552.
  • 4. Davies G.A.O., Hitchings D., Besant T., Clarke A., Morgan C., Compression after impact of composite sandwich panels, Composite Structures, 63 (2004), pp. l -9.
  • 5. Nemes J,A., Simmonds K.E., Low velocity impact response offoam-core sandwich composites, Journal of Composite Materials, 26(4) 1992, pp. 500-519.
  • 6. Shih W.K. Jang B.Z., Instrumented impact testing of composite sandwich panels, Journal of Reinforced Plastics and Composites, 8 (1989), pp. 270-298.
  • 7. Caprino G., Teti R., Impact and post-impact behaviour of foam core sandwich structures, Composite Structures, 29 (1994), pp. 47-55.
  • 8. Akay M, Hanna R., A comparison of honeycomb-core and foam-core carbon fibre/epoxy sandwich panels, Composites, 21(4) (1993), pp. 325-331
  • 9. Lendze T., Low-velocity impact damage and uhrasonic C-scan technique in glass/polyesler composite sandwich panels, Master degree diploma report, Gdańsk University of Technology, Universite Bordeaux, l, 2005.
  • 10. Imielińska K., Wojtyra R., Udarowe pękanie hybrydowych kompozytów epoksydowych zbrojonych włóknami szklanymi, węglowymi i aramidowymi, Inżynieria Materiałowa, 24 nr 3(134) (2003), pp. 127-134.
  • 11. Imielińska K., Castaings M., Wojtyra R., Haras J., Le Clezio E., Hosten B., Air-coupled uhrasonic C-scan technique in impact response testing of carbon fibre and hybrid: glass, carbon and Kevlar/epoxy composites, Journal of Materials Processing and Technology, 2004, Vol. 157-158, pp. 513-522.
  • 12. Castaings M., .Hosten B., Ultrasonics 36, 1-5 (1998) 361.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPG5-0016-0113
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