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The effect of the fiber orientation in a laminate is investigated experimentally when subjected repeated quasistatic indentation. All the laminates with different fiber orientation are subjected to indentation with a stainless steel spherical indenter of diameter 8.0mm on a universal testing machine for a maximum indenter displacement of 4mm. The rate of indenter displacement was 0.5mm/minute. Different parameters like load bearing capacity, indentation diameter, area of surface damage, etc., were recorded after 4mm of indenter displacement. All the parameters were studied and compared to evaluate the laminate with high strength.
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Czasopismo
Rocznik
Strony
46--56
Opis fizyczny
Bibliogr. 14 poz., rys., tab.
Twórcy
autor
- Vignan Institute of Technology & Science, Dept. of Mech. Eng., Hyderabad, Telangana, India
autor
- UCE, Osmania University, Dept. of Mech. Eng., Hyderabad, Telangana, India
autor
- TKR College of Engineering, Dept. of Mech. Eng., Hyderabad, Telangana, India
autor
- Vignan Institute of Technology & Science, Dept. of Mech. Eng., Hyderabad, Telangana, India
Bibliografia
- 1. Ross C.A., Sierakowski R.L., Studies on the impact resistance of Composite plates. Composites 4 (1973) 157-61.
- 2. Xiao J.R., Gama B.A., Gillespie Jr. J.W., Progressive damage and delamination in plain weave S-2 glass /SC-15 composites under quasi-static punch-shear loading. Composite struct., 78 (2007), 182-96.
- 3. AbiAbdallah, Christophe Bouvet. Experimental analysis of damage creation and permanent indentation on highly oriented plates, Composites science and Tech., 69, (2009), 1238-1245.
- 4. Crisfeld M.A., Mi Y, Davies Gao, Jellweg G.B., Finite element methods and the progressive failure modeling of composite structures. In Wen DRJ, et al., editor’s .Computational plasticity fundamentals and applications, CIMNE Barcelona; (1997), 239-54.
- 5. Li CF. Hu N. Cheng JG. Fukumaga H. Sekine H. Low velocity impact induced damage of continuous fiber reinforced composite laminates. Part-II Compos part-A, 33 (2002), 1063-72.
- 6. Mitrevski T. Marshall I.H., Thomson R., The influence of impactor shape on damage to composite laminates. Compos Struct., 76, (2006), 116-22.
- 7. Davies G.A.O., Zhang X., Impact damage prediction in carbon composite structures. Int. J. impact Eng., 16(1) (1995), 149-70.
- 8. Caprino G., Lopresto V., The significance of indentation in the inspection of carbon fibre reinforced plastic panels damaged by low-velocity impact. Compos. Sci. Technol., 60 (2000), 1003-12.
- 9. Caprino G., Lopresto V., Factors affecting the penetration energy of glass fiber reinforced plastics subjected to a concentrated transverse load. Proc. ECCM9, Brighton, UK; 4-7 June 2000
- 10. Caprino G., Lopresto V., The Penetration energy of fiber reinforced plastics under low-velocity impact conditions. Compos. Sci.Technol., 61 (2000), 65-73.
- 11. Freitas M., Silva A., Reis L., Numerical evaluation of failure mechanisms on composite specimens subjected to impact loading. Composite part B, 31 (3) (2000), 199-207.
- 12. Richardson M.O.W., Wiheart M.J., Review of low velocity impact properties of composite materials Composites, Part A -Appl, Sci. Manuf., 27A (12) (1996), 1123-31.
- 13. Wu E., Chang I.C., Woven glass/epoxy laminates subject to projectile impact, Int. J Impact Eng. 16 (4) (1995), 607-19.
- 14. Zhou G., Greaves I.J., Impact behavior of fiber reinforced composite materials and structures, CRC press, woodhead pubs., 2000, 133-185.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-297d5dfe-8388-458e-adcf-6adf35c96582