Fibre-metal laminates

Mohamed G, Soutis C, Hodzic A. Multi-material Arbitrary-Lagrangian-Eulerian formulation for blast-induced fluid-stmcture interaction in fibre metal laminates. AIAA J Am Inst Aeronaut Astronaut Struct Mech Mater 2012 50(9) 1826—33. [Pg.18]

McCarthy MA, Xiao JR, McCarthy CT, Kamoulakos A, Ramos J, Gallard JP, et al. Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates — part 2 modelling of impact with SPH bird model. Appl Compos Mater 2004 ... [Pg.293]

The blast response of composite and fibre-metal laminate materials used in aerospace applications... [Pg.371]

In this chapter, the characteristics of air explosions are briefly described and various blast protection paradigms are discussed. The blast behaviour of plain composites and multilayered structures are then discussed. Plain composites typically comprise polymeric resins with a fibre reinforcement, such as carbon fibre-reinforced epoxy resins. Multilayered systems include composite sandwich stmctures and hybrid composite-metal structures, known as fibre-metal laminates (FMLs). [Pg.371]

Figure 13.12 Photograph of a cross-section from a glass-fibre pol3fpropylene-based fibre-metal laminate panel subjected to uniformly distributed air-blast loading.

Guillen JF, Cantwell WJ. The influence of cooling rate on the fracture properties of a thermoplastic-based fibre-metal-laminates. J Reinf Plast Compos 2002 21(8) 749—72. [Pg.391]

Langdon GS, Cantwell WJ, Nurick GN. The blast response of novel thermoplastic-based fibre-metal laminates — some preliminary results and observations. Compos Sci Technol 2005 65(6) 861-72. [Pg.391]

Langdon GS, Nurick GN, Lemanski SL, Simmons MC, Cantwell WJ, Schleyer GK. Failure characterisation of blast-loaded fibre-metal laminate panels based on aluminium and glass-fibre reinforced polypropylene. Compos Sci Technol 2007 67(7-8) 1385-405. [Pg.391]

Langdon GS, Nurick GN, Cantwell WJ. The response of fibre-metal laminates subjected to uniformly distributed blast loading. Euro J Mech A Solids 2008 27(2) 107—15. [Pg.391]

Lemanski SL, Nurick GN, Langdon GS, Simmons MC, Cantwell WJ, Schleyer GK. Behaviour of fibre-metal laminates subjected to locahsed blast loading part II — quantitative analysis. Int J Impact Eng 2007 34(7) 1223—45. [Pg.391]

Karagiozova D, Langdon GS, Nurick GN. ModeUing the behaviour of fibre—metal laminates subjected to locahsed blast loading. In Reddy D, editor. Theoretical, model-hng and computational aspects of inelastic media. International Union of Theoretical and Apphed Mechanics 2008. pp. 319—28. [Pg.391]

Vo TP, Guan ZW, Cantwell WJ, Schleyer GK. Modelling of the low-impulse blast behaviour of fibre—metal laminates based on different aluminium alloys. Composites Part B 2012 44 141-51. [Pg.391]

Kuang KSC, Kenny R, Whelan MP, Cantwell WJ, ChaUcer PR. Residual strain measurement and impact response of optical fibre Bragg grating sensors in fibre metal laminates. Smart Mater Struct 2001 10(2) 338—46. http //dx.doi.org/10.1088/0964-1726/10/2/321. [Pg.502]

Vlot, A. GuNNINK, J.W. (Eds.) (2002) Fibre Metal Laminates. An Introduction. 444 pages ISBN 1-4020-0391-9. Vinson, J.R. Sierakowski, R.L. The Behavior of Structures Composed of Composite Materials. [Pg.1035]

Figure 25 Crack growth in fibre-metal laminates compared with aluminium alloy (courtesy of Fibre Metal Laminates, Delft).

Although aircraft structures comprise thousands of components produced from a myriad of basic materials, the most common substrates for structural adhesive bonding are wood, aluminium, titanium, stainless steel and the composite materials such as bonded sandwich structures, fibre reinforced plastic (FRP) laminates and fibre-metal laminates (FML) where the metal is usually aluminium. [Pg.244]

Mention has been made above of fibre-metal laminates. These are not only bonded structural substrates in their own right - the layers of aluminium and unidirectional fibres are joined together using a true adhesive matrix - but in... [Pg.313]

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