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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
... 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...
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Published: 01 December 2006
Fig. 33 Intergranular corrosion at the external surface of the flange. The voids are the locations of the spalled grains. 50× More
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Published: 01 March 2000
Fig. 6 Internal voids in 7016 bumper extrusion More
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Published: 01 March 2000
Fig. 7 Mechanism of internal voids More
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Published: 01 November 2010
Fig. 7.21 Interply and intraply voids and porosity More
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Published: 01 November 2010
Fig. 12.15 Voids in foaming adhesive More
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Published: 01 November 2010
Fig. 14.21 Various forms of voids and porosity More
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Published: 01 December 2004
Fig. 5.6 How shrinkage voids form in aluminum castings. (a) Initial void formation. (b) Collapse of shell increases void size. (c) “Wormhole” formation with additional shrinkage More
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Published: 01 November 2010
Fig. 1.7 Voids found in a glass fiber composite cross section due to solvents from manufacturing. Bright-field illumination, 10× objective More
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Published: 01 November 2010
Fig. 6.12 Voids in a glass-fiber-filled engineering thermoplastic matrix. Transmitted light, differential interference contrast, 40× objective More
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Published: 01 November 2010
Fig. 8.3 Voids in the interstitial areas of a plain weave carbon fiber composite. Bright-field illumination, 65 mm macrophotograph More
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Published: 01 November 2010
Fig. 8.4 Entrapped air voids in a tubular composite part made with unidirectional carbon fiber prepreg. Slightly uncrossed polarized light, 10× objective More
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Published: 01 November 2010
Fig. 8.5 Voids due to entrapped air shown in the interlayer region of a tubular composite part. (a) Section polished on a tangent to the outer radius. Slightly uncrossed polarized light, 10× objective. (b) Section polished on a tangent to the interior radius showing a similar fiber angle More
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Published: 01 November 2010
Fig. 8.6 Voids in the interlayer region and at the ply-drop in the interior of a tubular composite part. Bright-field illumination, 10× objective More
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Published: 01 November 2010
Fig. 8.8 Voids in a high-fiber-volume unidirectional carbon fiber composite part. (a) Sectioned and polished perpendicular to the fiber direction. Bright-field illumination, 10× objective. (b) Sectioned and polished parallel to the fiber direction. Bright-field illumination, 10× objective More
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Published: 01 November 2010
Fig. 8.9 Glass fabric prepreg honeycomb core composite with voids throughout the structure. Bright-field illumination, 5× objective More
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Published: 01 November 2010
Fig. 13.4 Solvent-generated voids in the prepreg skins and fillet areas of a honeycomb sandwich structure composite. (a and b) Bag side. (c) Tool side. Epi-bright-field illumination, 5× objective. In these micrographs, there is evidence of some scratching on the polished surface. This is due More
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Published: 01 December 2018
Fig. 6.15 (a) SEM fractograph showing presence of creep voids on fracture lip surface, 500×; and (b) SEM image of as-polished sample after metallography showing scattered creep voids, 1000× More
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Published: 01 December 2018
Fig. 6.40 SEM fractograph of the rupture surface showing scattered creep voids and cracks More
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Published: 30 November 2013
Fig. 4 Comparison of wedge-shaped cracks and creep voids: (a) triple-point stress rupture (60×); (b) creep cavitation damage (arrows) in a desuperheater inlet header (1000×) More