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epi-fluorescence

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Published: 01 November 2010
Fig. 9.12 Intraply microcracks in a carbon fiber composite material. Epi-fluorescence, 390–440 nm excitation, 25× objective More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030159
EISBN: 978-1-62708-349-2
... in a carbon fiber composite that is difficult to observe using bright-field illumination but easily identified after the application of a fluorescing dye (Magnaflux Zylgo, Magnaflux Corp.) and epi-fluorescence. (a) Bright-field illumination, 10× objective, with an inset showing the crack using epi...
Image
Published: 01 November 2010
Fig. 11.3 Impact damage of a carbon fiber composite material that has a brittle matrix. (a) Montage of the impact area. Epi-fluorescence, 390–440 nm excitation, 5× objective. (b) Fiber fracture area in the composite. Epi-fluorescence, 390–440 nm excitation, 25× objective. (c) Fracture shown More
Image
Published: 01 November 2010
Fig. 9.11 Intraply microcrack in a carbon fiber composite that is difficult to observe using bright-field illumination but easily identified after the application of a fluorescing dye (Magnaflux Zylgo, Magnaflux Corp.) and epi-fluorescence. (a) Bright-field illumination, 10× objective More
Image
Published: 01 November 2010
Fig. 11.4 Impact damage of a carbon fiber composite material that has a toughened matrix. (a) Montage of the impact area. Epi-fluorescence, 390–440 nm excitation, 5× objective. (b) Multiple intraply fractures. Epi-fluorescence, 390–440 nm excitation, 25× objective. (c) Adhesive failure More
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Published: 01 November 2010
Fig. 11.5 Impact damage of a carbon fiber composite material that has a toughened matrix. (a) Montage of the impact area. Epi-fluorescence, 390–440 nm excitation, 5× objective. (b) Wide crack formation in the 45° plies and mainly cohesive failure in the interlayer. Epi-fluorescence, 390–440 nm More
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Published: 01 November 2010
Fig. 9.14 Comparison of the same area in a carbon fiber composite using epi-bright-field illumination and epi-fluorescence. The microcracked area of the composite material was sectioned and polished at an oblique angle through the thickness to emphasize the interlayer region. (a) Bright-field More
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Published: 01 November 2010
Fig. 5.10 Microcracks in a composite material that are difficult to observe using epi-bright-field illumination. (a) Bright-field illumination, 25× objective. (b) Same location viewed after applying a fluorescent penetrant dye (Magnaflux Zyglo) to the surface and back-polishing. Epi More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030193
EISBN: 978-1-62708-349-2
...-dyed epoxy casting resin. The use of epi-bright-field illumination does not allow the dye to fluoresce, and therefore, the cracks are hard to distinguish. Bright-field montage, 5× objective Fig. 11.4 Impact damage of a carbon fiber composite material that has a toughened matrix. (a) Montage...
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Published: 01 November 2010
of the polished specimen, wiped off after 2 min, and cleaned with water. The solvent/dye preferentially absorbed into the particles and phases and not the thermoset matrix. Epi-fluorescence, 390–440 nm excitation, 25× objective More
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Published: 01 November 2010
present is a very small dispersed phase that fluoresces yellow. Epi-fluorescence, 390–440 nm excitation, 25× objective More
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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 More
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Published: 01 November 2010
of the specimen to enhance the contrast of the microcracks. Epi-fluorescence, 390–440 nm excitation, 10× objective More
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Published: 01 November 2010
× objective. (b) Dark-field illumination, 25× objective. (c) Polarized light, 25× objective. (d) Slightly uncrossed polarized light, 25× objective. (e) Epi-fluorescence, 390–440 nm, 25× objective. (f) Transmitted light, Hoffman modulation contrast, 20× objective More
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Published: 01 November 2010
Fig. 9.13 Large-scale microcracking in a carbon fiber composite material. Epi-fluorescence, 390–440 nm excitation, 10× objective More
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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 More
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Published: 01 November 2010
Fig. 15.5 Micrograph taken under the strike zone showing damage induced by the lightning strike. Epi-fluorescence, 390–440 nm excitation, 25× objective More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030245
EISBN: 978-1-62708-349-2
... zone corresponding to section plane A in Fig. 15.1 . The micrographs are taken away from the main damage area to show the effects of interply arcing. A Kevlar stitch is shown between the carbon fibers. (a) Slightly uncrossed polarized light, 25× objective. (b) Epi-fluorescence, 390–440 nm excitation...
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Published: 01 November 2010
Fig. 15.4 Micrograph taken at an area under the lightning strike zone showing delamination and microcracking in the composite. Epi-fluorescence, 390–440 nm excitation, 10× objective More
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Published: 01 November 2010
, and then subjected to the last stage of polishing to remove additional dye from the surface. Epi-fluorescence, 390–440 nm excitation, 50× objective More