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| Author | : Bing Kang Yen |
| Publisher | : |
| Total Pages | : 320 |
| Release | : 1991 |
| Genre | : |
| ISBN | : |
| Author | : Christos C. Chamis |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1970 |
| Genre | : Fibrous composites |
| ISBN | : |
| Author | : Minoru Taya |
| Publisher | : Elsevier |
| Total Pages | : 275 |
| Release | : 2016-01-11 |
| Genre | : Technology & Engineering |
| ISBN | : 1483191133 |
Metal Matrix Composites: Thermomechanical Behavior discusses metal matrix composites, elaborating on that consists of two phases—fiber as reinforcement and metal as matrix. This book focuses on polymer matrix composites, including topics in metal matrix composites ranging from processing to fracture mechanics. The three basic types of composite materials—dispersion-strengthened, particle-reinforced, and fiber (whisker)-reinforced, are also described in detail. Dispersion-strengthened is characterized by a microstructure consisting of an elemental matrix within which fine particles are uniformly dispersed, while particle-reinforced is indicated by dispersed particles of greater than 1.0 μm diameter with a volume fraction of 5 to 40%. Fiber (whisker)-reinforced provides a distinguishing microstructural feature of fiber-reinforced materials, such as that the reinforcing fiber has one long dimension, while the reinforcing particles of the other two types do not. This publication serves as a reference data book to students and researchers aiming to acquire knowledge of the thermomechanical behavior of metal matrix composites.
| Author | : Clifford Jesse Lissenden |
| Publisher | : |
| Total Pages | : 212 |
| Release | : 1993 |
| Genre | : |
| ISBN | : |
| Author | : W. Steven Johnson |
| Publisher | : ASTM International |
| Total Pages | : 289 |
| Release | : 1989 |
| Genre | : Fracture mechanics |
| ISBN | : 080311270X |
Fourteen peer-reviewed papers on testing techniques, analysis approaches, and descriptions of various failure processes. From the Symposium on [title] held at Sparks, NV, April 1988. Annotation copyright Book News, Inc. Portland, Or.
| Author | : |
| Publisher | : |
| Total Pages | : 546 |
| Release | : 1994 |
| Genre | : |
| ISBN | : |
This document discusses the following: (1) Materials selection and innovation in design; (2) Elasto-plastic analysis of interface layers for fiber- reinforced metal-matrix composites; (3) Modeling of anisotropic behavior of weakly bonded fiber reinforced MMCs; (4) On the tensile properties of a fiber reinforced titanium matrix composite; (5) Control of strength anisotropy of metal matrix fiber composites; (6) inelastic strains due to matrix cracking in unidirectional fiber-reinforced composites; (7) Location and ultimate tensile strength of fiber-reinforced ceramic-matrix composites; (8) Matrix cracking and debonding of ceramic-matrix composites; (9) Matrix cracking of cross-ply ceramic composites; (10) Transverse cracking in fiber-reinforced brittle matrix, cross- ply laminates; (11) The mechanisms of deformation and failure in carbon matrix composites subject to tensile and shear loading; (12) Uncoupled and coupled approaches to predict crack-initiation in fiber-reinforced ceramic-matrix composites; (13) Stress corrosion cracking in a unidirectional ceramic-matrix composite; (14) Effects of gauge length on the tensile strength of SiC fibers; (15) Tunneling cracks in constrained layers; (16) The effect of interfacial properties on the flow strength of discontinuous reinforced metal matrix composites; (17) On dislocation storage and the mechanical response of fine scale microstructures; and (18) Effect of microstructural parameters on the yield strength of Al-4%Mg/Al2O3p composites.
| Author | : P.K. Mallick |
| Publisher | : CRC Press |
| Total Pages | : 1262 |
| Release | : 1997-03-19 |
| Genre | : Technology & Engineering |
| ISBN | : 1482277735 |
Offers information on the fundamental principles, processes, methods and procedures related to fibre-reinforced composites. The book presents a comparative view, and provides design properties of polymeric, metal, ceramic and cement matrix composites. It also gives current test methods, joining techniques and design methodologies.
| Author | : GM. Newaz |
| Publisher | : |
| Total Pages | : 14 |
| Release | : 1996 |
| Genre | : Ceramic fibers testing |
| ISBN | : |
An investigation was undertaken to evaluate the constitutive response and in-elastic deformation characteristics in titanium-based metal matrix composites (MMC) with two types of ceramic fibers, namely, SCS-6 and Sigma. The titanium matrix was Beta 21S, currently named TIMETAL-21S. Monotonic tests were conducted at room temperature (RT) and between 483 and 815°C. The inelastic deformation in the [0]8 lamina under compression was controlled primarily by matrix plasticity, although some evidence of fiber-matrix debonding was observed. The inelastic deformation mechanisms under compression in [90]8 lamina were primarily due to radial fiber cracking from the core for the SCS-6 fiber and fiber-matrix debonding. However, for the Sigma fiber, radial cracking was absent. The effect of temperature on degradation of mechanical properties such as modulus and yield strength for the composites with two different fibers were compared.
| Author | : National Aeronautics and Space Administration (NASA) |
| Publisher | : Createspace Independent Publishing Platform |
| Total Pages | : 50 |
| Release | : 2018-07-05 |
| Genre | : |
| ISBN | : 9781722363963 |
The nonlinear anisotropic mechanical behavior of an aluminum alloy metal matrix composite reinforced with continuous alumina fibers was determined experimentally. The mechanical behavior of the composite were modeled by assuming that the composite has a periodical microstructure. The resulting unit cell problem was solved with the finite element method. Excellent agreement was found between theoretically predicted and measured stress-strain responses for various tensile and shear loadings. The stress-strain responses for transverse and inplane shear were found to be identical and this will provide a simplification of the constitutive equations for the composite. The composite has a very low ductility in transverse tension and a limited ductility in transverse shear that was correlated to high hydrostatic stresses that develop in the matrix. The shape of the initial yield surface was calculated and good agreement was found between the calculated shape and the experimentally determined shape. Jansson, S. Unspecified Center NAG3-894; RTOP 510-01-50...
| Author | : |
| Publisher | : |
| Total Pages | : 426 |
| Release | : 1995 |
| Genre | : Aeronautics |
| ISBN | : |
