2003
DOI: 10.1023/a:1025569316827
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Cited by 61 publications
(25 citation statements)
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“…It takes advantages of both metals and fiber-reinforced composites, providing superior mechanical properties that cannot be achieved by either of its constituents [3,4]. Major advantages of GLARE include low density, high fracture toughness and strength [5,6], high impact [7] and fatigue resistance [8], excellent moisture and corrosion resistance [9], etc. Due to the advantages listed above, GLARE is being sought after for more applications in the aerospace industry.…”
Section: Introductionmentioning
confidence: 99%
“…It takes advantages of both metals and fiber-reinforced composites, providing superior mechanical properties that cannot be achieved by either of its constituents [3,4]. Major advantages of GLARE include low density, high fracture toughness and strength [5,6], high impact [7] and fatigue resistance [8], excellent moisture and corrosion resistance [9], etc. Due to the advantages listed above, GLARE is being sought after for more applications in the aerospace industry.…”
Section: Introductionmentioning
confidence: 99%
“…Carall is a hybrid material, which consist of thin aluminum 2024-T3 metal sheets bonded together with alternating carbon fiber/epoxy layers. This hybrid material presents superior mechanical properties over the conventional polymer composite laminates and monolithic aluminum alloy [5][6][7][8][9][10][11][12][13].…”
mentioning
confidence: 99%
“…The classic laminate theory has been modified to predict the linear-elastic and elastic-plastic behavior of the FMLs [5,9]. The modified classical laminate theory is adopted in order to obtain the stress-strain response of hybrid FMLs.…”
Section: Modified Classical Laminate Theorymentioning
confidence: 99%
“…Nevertheless, S-2 glass fiber used in the current generation of the Glare laminate has a high tensile strength and strain-to-failure. The combination of lower modulus S-2 glass/epoxy prepreg layers and aluminum sheets inevitably produce a laminate with a Young's modulus lower than that of the monolithic aluminum alloy [5]. This may limit the applications of the Glare laminates in aircraft structures where the stiffness is a predominant design requirement.…”
Section: Introductionmentioning
confidence: 99%