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Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030001
EISBN: 978-1-62708-349-2
... Abstract This chapter provides a general description of materials and methods for manufacturing high-performance composites. The materials covered are polymer matrices and prepreg materials and the methods include infusion processes, composite-toughening methods, matrix-toughening methods...
Abstract
This chapter provides a general description of materials and methods for manufacturing high-performance composites. The materials covered are polymer matrices and prepreg materials and the methods include infusion processes, composite-toughening methods, matrix-toughening methods, and dispersed-phase toughening. In addition, the chapter provides information on interlayer-toughened composites and honeycomb or foam structure composite materials. It also discusses the processes in optical microscopy of composite materials.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030147
EISBN: 978-1-62708-349-2
... that occur in honeycomb core composites. The final section of the chapter discusses void documentation through the use of nondestructive inspection techniques and density/specific gravity measurement methods. composite materials honeycomb core composites ply-drops void analysis Achieving...
Abstract
Achieving the best-performing composite part requires that the processing method and cure cycle create high-quality, low-void-content structures. If voids are present, the performance of the composite will be significantly reduced. There are multiple causes of voids in composite materials; they are generally categorized as voids that are due to volatiles (such as solvents, water) or voids that result from entrapped air. This chapter describes the analysis of various types of voids. It reviews techniques for analysis of voids at ply-drops, voids due to high fiber packing, and voids that occur in honeycomb core composites. The final section of the chapter discusses void documentation through the use of nondestructive inspection techniques and density/specific gravity measurement methods.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030159
EISBN: 978-1-62708-349-2
... Abstract The formation of microcracks in composite materials may arise from static-, dynamic-, impact-, or fatigue-loading situations and also by temperature changes or thermal cycles. This chapter discusses the processes involved in the various methods for the microcrack analysis of composite...
Abstract
The formation of microcracks in composite materials may arise from static-, dynamic-, impact-, or fatigue-loading situations and also by temperature changes or thermal cycles. This chapter discusses the processes involved in the various methods for the microcrack analysis of composite materials, namely bright-field analysis, polarized-light analysis, contrast dyes analysis, and dark-field analysis. The analysis of microcracked composites using epi-fluorescence is also covered. In addition, the chapter describes the procedures for the determination and recording of microcracks in composite materials.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870001
EISBN: 978-1-62708-314-0
... Abstract This chapter covers the basic aspects of composite materials. It describes the arrangement, form, and function of their constituent materials and explains how they perform better in combination than on their own. It discusses the directional nature of isotropic, anisotropic...
Abstract
This chapter covers the basic aspects of composite materials. It describes the arrangement, form, and function of their constituent materials and explains how they perform better in combination than on their own. It discusses the directional nature of isotropic, anisotropic, and orthotropic materials, the orientation of plies in unidirectional (lamina) and quasi-isotropic (laminate) lay-ups, and the dominant role of fibers in determining strength, stiffness, and other lamina properties. The chapter also compares the engineering attributes of composites with those of metals and includes application examples.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.9781627083140
EISBN: 978-1-62708-314-0
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Published: 01 December 2006
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Published: 01 December 2006
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Published: 01 December 2006
Fig. 5.91 Property comparison between Cu/Pd composite materials (VW) and corresponding Pd/Cu alloys (electrical conductivity and hardness after cold working)
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in Introduction—Composite Materials and Optical Microscopy
> Optical Microscopy of Fiber-Reinforced Composites
Published: 01 November 2010
Fig. 1.2 Composite materials made from different types of fibers. (a) Woven glass fiber fabric composite revealing a multiphase-matrix morphology. Ultrathin section, transmitted-light phase contrast, 20× objective. (b) Kevlar (E.I. du Pont de Nemours and Company) fabric composite cross section
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in Introduction—Composite Materials and Optical Microscopy
> Optical Microscopy of Fiber-Reinforced Composites
Published: 01 November 2010
Fig. 1.11 Cross sections of interlayer-modified composite materials. (a) Cross section showing a middle ply at 90°. Bright-field illumination, 10× objective. (b) Cross section taken parallel to the fiber direction. Bright-field illumination, 10× objective
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Published: 01 November 2010
Fig. 2.12 The most useful cavity mold type for mounting composite materials. A single mold can last for many samples. Each time one is used, it should be release-coated for easy sample removal and extended life. For producing samples for transmitted-light analysis ( Chapter 6 ), this mold
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Published: 01 November 2010
Fig. 2.14 Photograph of mounted composite materials after removal from a rubber mold. This figure shows a polished top surface.
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Published: 01 November 2010
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Published: 01 June 1983
Figure 2.20 Specific heat as a function of temperature for five composite materials. The true shapes of the fiber-reinforced composite curves are somewhat uncertain because of the widely spaced data points. The calculated values for the polystyrene foam are based on 98 wt.% polystyrene and 2
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Published: 01 June 1983
Figure 3.29 Thermal expansion vs. temperature for some composite materials compared with calculated values.
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Published: 01 December 2006
Fig. 5.83 Structure of extruded copper/palladium-composite material. Micrograph image width is approximately 3.6 mm
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in Introduction—Composite Materials and Optical Microscopy
> Optical Microscopy of Fiber-Reinforced Composites
Published: 01 November 2010
Fig. 1.9 Thermoplastic stitch in carbon fiber composite material. Note the microcracks in the center of the stitch. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Published: 01 November 2010
Fig. 2.1 Coordinates defined for composite material sample preparation as related to sectioning and viewing planes. Sectioning through the composite thickness on an angle helps in determining ply orientations (i.e., fibers will become elongated).
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Published: 01 November 2010
Fig. 2.5 Composite material that was cut using a waterjet. Very little damage is observed at the cut edge of the specimen. A fluorescing dye was applied to the cut edge to determine if cracks were present. Epi-fluorescence, 390–440 nm excitation, 25× objective
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Published: 01 November 2010
Fig. 2.6 Cut edge of a composite material after sectioning with an abrasive cut-off saw. The composite was mounted using a Rhodamine-B-dyed epoxy resin and viewed using epi-fluorescence, 390–440 nm excitation, 25× objective.
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