2005
DOI: 10.1007/s11837-005-0067-4
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The mechanical behavior of GLARE laminates for aircraft structures

Abstract: GLARE (glass-reinforced aluminum laminate) is a new class of fi ber metal laminates for advanced aerospace structural applications. It consists of thin aluminum sheets bonded together with unidirectional or biaxially reinforced adhesive prepreg of high-strength glass fi bers. GLARE laminates offer a unique combination of properties such as outstanding fatigue resistance, high specific static properties, excellent impact resistance, good residual and blunt notch strength, fl ame resistance and corrosion propert… Show more

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Cited by 288 publications
(177 citation statements)
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“…As special sandwich structures, fiber-metal laminates (FML) are layered materials based on stacked arrangements of FRP layers such as glass fiber-reinforced epoxy resin and thin metal sheets such as aluminium or titanium alloys. 19,20 Compared to the monomaterials used, Al and FRP-FML show an improved behavior. 21,22 They exhibit excellent fatigue and high-specific-static properties as well as an improved impact resistance, flame resistance and ease of manufacture and repair.…”
Section: Industrial Sandwichesmentioning
confidence: 99%
“…As special sandwich structures, fiber-metal laminates (FML) are layered materials based on stacked arrangements of FRP layers such as glass fiber-reinforced epoxy resin and thin metal sheets such as aluminium or titanium alloys. 19,20 Compared to the monomaterials used, Al and FRP-FML show an improved behavior. 21,22 They exhibit excellent fatigue and high-specific-static properties as well as an improved impact resistance, flame resistance and ease of manufacture and repair.…”
Section: Industrial Sandwichesmentioning
confidence: 99%
“…Fatigue tests and fatigue modeling on fiber reinforced composites for wind blades are normally up to a few million cycles. A typical fibermetal laminate such as GLARE was developed about thirty years ago and successfully applied in the fuselage skin for Airbus 380 [8] due to its low specific weight and high fatigue strength compared with pure alloy materials [9]. The main reason of the high fatigue probability for GLARE is the fiber bridging effect to restraint the crack tip opening at the aluminum layers to reduce the stress intensity factor and decrease the crack growth rate [10].…”
Section: Introductionmentioning
confidence: 99%
“…Incorporating composite layers into a metal sheets system greatly enhances the overall performance of the FML which combines the advantages of both conventional composites and metals. In previous studies, FML has been proved to have many excellent mechanical properties such as outstanding fatigue resistance, high specific static properties, superior impact resistance, good residual and blunt notch strength, better bearing strength, fire resistance and corrosion properties [2]. Currently, glass-reinforced aluminium laminate (GLARE) has been selected for the upper fuselage skin structures of Airbus A380, as shown in Figure 1 [3].…”
Section: Introductionmentioning
confidence: 99%