1-20 of 42 Search Results for

epi-fluorescence

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Image
Published: 01 December 2004
Fig. 12 Intraply microcracks in a carbon fiber composite material. Epi-fluorescence, 390–440 nm excitation, 25× objective More
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003464
EISBN: 978-1-62708-195-5
...-fluorescence. The article also provides information on transmitted light microscopy. composite materials epi-bright-field illumination epi-dark-field illumination epi-fluorescence epi-polarized light failure analysis illumination methods mounting polishing quality control reflected light...
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009079
EISBN: 978-1-62708-177-1
... Abstract This article describes the microcrack analysis of composite materials using bright-field illumination, polarized light, dyes, dark-field illumination, and epi-fluorescence. bright-field illumination composite materials dark-field illumination dyes epi-fluorescence microcrack...
Image
Published: 01 December 2004
Fig. 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 December 2004
Fig. 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 December 2004
Fig. 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
Image
Published: 01 December 2004
Fig. 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
Image
Published: 01 December 2004
Fig. 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
Image
Published: 01 December 2004
Fig. 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-fluorescence More
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009081
EISBN: 978-1-62708-177-1
... the origin and extent of the damage in the composite. To better identify the location of the damage in the intra- and interlayer areas, greater contrast may be required. In this case, epi-fluorescence can prove to be very valuable. Further information regarding the effect on the matrix microstructure...
Image
Published: 01 December 2004
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
Image
Published: 01 December 2004
present is a very small dispersed phase that fluoresces yellow. Epi-fluorescence, 390–440 nm excitation, 25× objective More
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009085
EISBN: 978-1-62708-177-1
..., including polarized light, bright- and dark-field illumination, and epi-fluorescence. The damage characteristics depend on many factors, including the type of lightning strike protection material on the surface (expanded foil or interwoven wire), the polymer matrix, the fiber type and volume, the lay-up...
Image
Published: 01 December 2004
Fig. 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
Image
Published: 01 December 2004
to enhance the contrast of the microcracks. Epi-fluorescence, 390–440 nm excitation, 10× objective More
Image
Published: 01 December 2004
× 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
Image
Published: 01 December 2004
Fig. 13 Large-scale microcracking in a carbon fiber composite material. Epi-fluorescence, 390–440 nm excitation, 10× objective More
Image
Published: 01 December 2004
, 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
Image
Published: 01 December 2004
Fig. 9 Thermoplastic stitch in carbon fiber composite material. Note the microcracks in the of the stitch. Epi-fluorescence, 390–440 nm excitation, 25× objective More
Image
Published: 01 December 2004
Fig. 5 Micrograph taken under the strike zone showing damage induced by the lightning strike. Epi-fluorescence, 390–440 nm excitation, 25× objective More