Multiple impact effects of helium-driven shocks on thin fiber-metal laminates. [PDF]
Pai A +3 more
europepmc +1 more source
Tensile and compressive test results for metal matrix composites [PDF]
Experimental results of the mechanical behavior of two metal matrix composite systems at room temperature are presented. Ultimate stress, ultimate strain, Poisson's ratio, and initial Young's Modulus are documented for BORSIC/Aluminum in uniaxial tension
Herakovich, C. T., Shuart, M. J.
core +1 more source
Investigation on Formability of Fiber Metal Laminates
In this study, the formability of fiber metal laminates (FML) used in aerospace industry were experimentally examined. Al5754-H22 sheets in two different thicknesses (0.6 and 1.2 mm) were used in top and bottom layers of FML specimens. Carbon fiber plates made of prepreg carbon fiber fabrics were placed in the middle layer of FML specimens. In order to
IŞIKTAŞ, Ali, TAŞKIN, Vedat
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Microfracture in high temperature metal matrix laminates [PDF]
Computational simulation procedures are described to evaluate the composite microfracture behavior, establish the hierarchy/sequence of fracture modes, and the influence of compliant layers and partial debonding on composite properties and microfracture ...
Chamis, Christos C. +2 more
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A tenacidade à fratura translaminar dinâmica do laminado híbrido metal-fibra titânio-grafite com matriz termoplástica foi determinada sob as velocidades de impacto de 2,25 e 5,52 m/s, no intervalo de temperaturas de -196 a +180 °C, e comparada à de ...
José R. Tarpani, Maria C. A. Gatti
doaj
Theoretical Modeling and Experimental Verification of the Bending Deformation of Fiber Metal Laminates. [PDF]
Chen Y, Wang Z, Lin Y, Wang H, Hua L.
europepmc +1 more source
Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum [PDF]
The influence of temper condition on the tensile and compressive stress-strain behavior for six boron-aluminum laminates was investigated. In addition to monotonic tension and compression tests, tension-tension, compression-compression, and tension ...
Herakovich, E. T. +2 more
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As a new type of aviation material,fiber/aluminum-lithium(Al-Li)laminates are significantly threatened by fatigue cracks. In other words,fatigue cracks are the “fatal killers”,which leads to their failure.
HUANG Xiao +4 more
doaj +1 more source
Microcapsules in Fiber Metal Laminates for Self-Healing at the Interface between Magnesium and Carbon Fiber-Reinforced Epoxy. [PDF]
Ostapiuk M.
europepmc +1 more source
Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites. Phase 3: Major component development [PDF]
Analytical and experimental investigations, performed to establish the feasibility of reinforcing metal aircraft structures with advanced filamentary composites, are reported.
Bryson, L. L., Mccarty, J. E.
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