Experimental investigation of repeated low velocity impact on GLARE with various energy levels

Authors

PhD Student, Mech. Eng., K.N.ToosiUniv. of Tech., Tehran, Iran

Abstract

In this study, an experimental investigation of repeated low velocity impact is performed on GLARE using drop weight testing machine. After the first impact on the plate, the second impact energy decreases and stays constant until the last impact. Damage due to repeated impact is investigated using visual inspection and C-scan. Three categories namely, no damage, small damage and serious damage are happened as a result of the first impact on the plate. The number of impacts required for the penetration is increased with decrease of the second impact energy. The threshold limit energy is defined as the maximum impact energy in repeated impact after the first impact which causes no damage on the specimen. For the successive impact energy larger than the threshold limit energy, the number of impacts becomes important, while for the successive impacts energies smaller than threshold limit energy, the number of impact has inconsiderable effect on damage occurrence.

Keywords

Main Subjects


[1] Vlot A, Gunnink JW (2001) Fiber Metal Laminates: an Introduction. Boston, Kluwer Academic Publishers, The Netherlands.
[2] Vermeeren CAJR (2003) An historic overview of the development of fibre metal laminates. Appl Compo Material 10: 189–205.
[3] Vermeeren CAJR, Beumler Th, De Kanter JLCG, Van Der Jagt OC, Out BCL (2003) Glare design aspects and philosophies. Appl Compo Materials 10: 257–276.
[4] Marissen R (1984) Fatigue Crack Growth in ARALL, A Hybrid Aluminium-Aramid Composite Material: Crack Growth Mechanisms and Quantitative Predictions of the Crack Growth Rates. Ph.D. Thesis. Delft University of Technology.
[5] Tsartsaris N, Meo M, Dolce F, Polimeno U, Guida M, Marulo F (2011) Low-velocity impact behavior of fiber metal laminates. J Compo Materials 45(7): 803-814.
[6] Vlot A, Vogelesang LB, De Vries TJ (1999) Towards application of fibre metal laminates in large aircraft. Aircraft Eng Aero Technology 71(6): 558–570.
[7] Alderliesten R, Rans C (2009) The meaning of threshold fatigue in fibre metal laminates. Int J Fatigue 31: 213–222.
[8] Abdullah MR, Cantwell WJ (2006) The impact resistance of polypropylene-based fibre-metal laminates. Compo Sci Technology 66: 1682–1693.
[9] Vlot A (1991) Low-velocity impact loading on fibre reinforced aluminium laminates (ARALL) and other aircraft sheet materials. Dissertation, Delft University of Technology, The Netherlands.
[10] Vlot A (1996) Impact loading on fiber metal laminates. Int J Imp Engineering 18(3): 291–307.
[11] Vlot A, Kroon E, Rocca GL (1998) Impact response of fiber metal laminates. Key Eng Material 141: 235–76.
[12] Fahr A, Chapman CE, Forsyth DS, Poon C, Laliberté JF (2000) Non-destructive evaluation methods for damage assessment in fiber-metal laminates. Poly Composite 21: 568–575.
[13] Laliberté JF, Poon C, Straznicky PV, Fahr A (2000) Applications of fiber-metal laminates. Poly Composites 21(4) :558–567.
[14] Liu Y, Liaw B (2010) Effect of constituents and lay-up configuration on drop-weight tests of fiber metal laminates. Appl Compo Materials 17(1): 43-62.
[15] Seyed Yaghoubi A, liu Y, Liaw B (2012) low velocity impact on glare 5 fiber metal laminate: influence of specimen Thickness and Impactor Mass. J Aero Engineering 25(3): 409-420.
[16] Vlot A, Krull M (1997) Impact damage resistance of various fibre metal laminates. J Physics 7(3): 1045-1050.
[17] Rajkumar GR, Krishna M, Narasimha Murthy HN, Sharma SC, Vishnu Mahesh KR (2012) Experimental investigation of low velocity Repeated impacts on glass fiber metal composites. JMEPEG 21(7): 1485-1490.
[18] Rajkumar GR, Krishna M, Narasimha Murthy HN, Sharma SC, Vishnu Mahesh KR (2012) Investigation of Repeated low velocity impact behavior of GFRP/Aluminium and CFRP / Aluminium Laminates. Int J Sof Compu Engineering 1(6): 50-58.
[19] Moriniere FD, Alderliesten RC, Yarmohammad Tooski M, Benedictus R (2012) Damage Evolution in GLARE-Fiber-Metal Laminate under Repeated Low-Velocity Impact Tests. Cent Euro Engineering 2(4): 603-611.
[20] Yarmohammad Tooski M, Alderliesten RC, Ghajar R, Khalili SMR (2013) Experimental investigation on distance effects in repeated low velocity impact on Fiber-Metal Laminates. Compo Structure 99: 31-40.