The blast response of novel thermoplastic-based fibre-metal laminates – some preliminary results and observations

This paper investigates the blast response of fibre-metal laminates (FMLs) manufactured from two glass fibre reinforced polypropylene composites and that of a plain aluminium alloy. The FMLs were manufactured by stacking the materials in a mould and applying heat and pressure to them. An autoclave was not used. In this work, attention focuses on elucidating the failure modes in the hybrid laminates. The blast data is non-dimensionalised to develop an empirical formula that characterises the behaviour of these materials under this extreme form of loading. The results indicate that thermoplastic-based FML materials may show potential for use in blast-resistant structures, due to their ability to absorb blast energy through delamination, debonding between the aluminium and composite layers, spalling/petalling of the aluminium, perforation through the layers and bending and stretching of the glass fibres. The tests also highlight the difference in response between panels constructed using woven (symmetrical response) and unidirectional (asymmetric behaviour) GFPP composites. The non-dimensional analysis appears to show that there is correlation between the response of all three panel types.

[1]  Genevieve Langdon,et al.  Experimental and numerical studies on the response of quadrangular stiffened plates. Part II: localised blast loading , 2005 .

[2]  W. Cantwell,et al.  The Influence of Cooling Rate on the Fracture Properties of a Thermoplastic-Based Fibre-Metal Laminate , 2002 .

[3]  G. Nurick,et al.  Tearing of blast loaded plates with clamped boundary conditions , 1996 .

[4]  N. Jacob,et al.  Scaling aspects of quadrangular plates subjected to localised blast loads—experiments and predictions , 2004 .

[5]  G. Nurick,et al.  The deformation and tearing of thin square plates subjected to impulsive loads—An experimental study , 1996 .

[6]  S. Chung Kim Yuen,et al.  Experimental and numerical studies on the response of quadrangular stiffened plates. Part I: subjected to uniform blast load , 2005 .

[7]  T. Wierzbicki Petalling of plates under explosive and impact loading , 1999 .

[8]  Wesley J. Cantwell,et al.  The mechanical properties of fibre-metal laminates based on glass fibre reinforced polypropylene , 2000 .

[9]  J. B. Martin,et al.  Deformation of thin plates subjected to impulsive loading—A review , 1989 .

[10]  G. Nurick,et al.  The deformation and tearing of thin circular plates subjected to impulsive loads , 1990 .

[11]  S. B. Menkes,et al.  Broken beams , 1973 .

[12]  G. Nurick,et al.  Some Insights Into The Mechanism Of TheDeformation And Tearing Of Thin Plates At HighStrain Rates Incorporating TemperatureDependent Material Properties , 2000 .

[13]  H. J. Fleisher,et al.  Design and explosive testing of a blast resistant luggage container , 1970 .

[14]  Gerald Nurick,et al.  Experimental investigation into the response of chopped-strand mat glassfibre laminates to blast loading , 2002 .

[15]  W. Cantwell,et al.  The Influence of a Fiber-Matrix Coupling Agent on the Properties of a Glass Fiber / Polypropylene GMT , 1992 .

[16]  W. Cantwell,et al.  Fracture of glass/polypropylene laminates: influence of cooling rate after moulding , 1994 .