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Photograph of cross-section

Figure 14.23 Photographs of cross-sectional views of resin removed from a Maddock solidification experiment for a Stratablend screw. The labels are the axial positions of the views in diameters... Figure 14.23 Photographs of cross-sectional views of resin removed from a Maddock solidification experiment for a Stratablend screw. The labels are the axial positions of the views in diameters...
Figure 9-12. a) Scheme of the internal solid state reaction CaO +Ti02 = CaTi03 in the matrix crystal NiO. Concentration profiles and precipitate are indicated, b) Photograph of cross section with internal reaction zone (T = 1340 C, t = 413 h reaction time). [Pg.230]

Figure 1 shows SEM photographs of cross sectional iracture of the Feo.9jSi2.oMno,)j thick films. The melting temperature seems to be approximately 1483 K. Table 1 shows the porosity of the films. The porosity is larger than 21 vol. % at 1478 K, while porosity decreases to 0 vol. % when the film was melted at 1483 K. These results show that the substrate restricts shrinkage of the film. The porosity can be decreased down to 8 vol. % when the film is melted. [Pg.634]

Fig. 3.11. Photograph of cross-section of broken 4BS crystal with PbS04 layer on surface [13]. Fig. 3.11. Photograph of cross-section of broken 4BS crystal with PbS04 layer on surface [13].
Fig. 3.45. Photographs of cross-section of negative plate during formation (a) prior to formation (b)-(d) during different formation stages, dark regions are Pb- -PbS04 zones (e) completely formed plate [56], Plate thickness is 1.8 mm. This is a vertical cross-section of the plate. Fig. 3.45. Photographs of cross-section of negative plate during formation (a) prior to formation (b)-(d) during different formation stages, dark regions are Pb- -PbS04 zones (e) completely formed plate [56], Plate thickness is 1.8 mm. This is a vertical cross-section of the plate.
Figure 13.11 Photographs of cross-sections from fihre-metal laminate (FML) panels subjected to localised air-hlast loading (a) 2/1 FML with unidirectional glass-fibre polypropylene (GFPP) layers, (b) 2/1 FML with unidirectional GFPP layers, (c) 2/1 FML with woven GFPP layers, (d) 3/2 FML with woven GFPP layers. Figure 13.11 Photographs of cross-sections from fihre-metal laminate (FML) panels subjected to localised air-hlast loading (a) 2/1 FML with unidirectional glass-fibre polypropylene (GFPP) layers, (b) 2/1 FML with unidirectional GFPP layers, (c) 2/1 FML with woven GFPP layers, (d) 3/2 FML with woven GFPP layers.
Fig. 6.1. FE-SEM photographs of cross sections of asymmetric 6FDA-BAAF membranes quenched in water at 30 °C and at 38 °C. Reprinted from [1 ]. Copyright 1999, with kind permission from the American Chemical Society... Fig. 6.1. FE-SEM photographs of cross sections of asymmetric 6FDA-BAAF membranes quenched in water at 30 °C and at 38 °C. Reprinted from [1 ]. Copyright 1999, with kind permission from the American Chemical Society...
Figure 4. SEM photograph of cross-section of the membrane prepared from the oriented-CyD-polymer on a filter paper as a support (x 1200). Figure 4. SEM photograph of cross-section of the membrane prepared from the oriented-CyD-polymer on a filter paper as a support (x 1200).
FIGURE 1.1.9 Photograph of cross-sectional SEM of solder joints of TCT (—40 to 123°C) samples of wire bonded chip assembly type CSP made of the 11.3 ppm/° C material after 1000 cycles. [Pg.12]

Figure 2 (a) SEM photographs of cross-sections of PP fibers with a linear density of 27 dtex. (b) SEM photograph of hollow-additivated FP fibers with linear density of 30 dtex. [Pg.756]

Figure 4. Photograph of cross-sections of polyurethane samples prepared in a microgravity environment at 1 atmosphere in a soundirig rocket experiment (right) compared to its ground-based comparison (left). Figure 4. Photograph of cross-sections of polyurethane samples prepared in a microgravity environment at 1 atmosphere in a soundirig rocket experiment (right) compared to its ground-based comparison (left).
Figure 18.2 Photographs of cross-section areas of (a) geotextile-geonet composites and (b) geotextile—geospacer. Figure 18.2 Photographs of cross-section areas of (a) geotextile-geonet composites and (b) geotextile—geospacer.
Figure 18.5 Photograph of cross-sectional area of a geotextile—geomemhrane composite. Figure 18.5 Photograph of cross-sectional area of a geotextile—geomemhrane composite.
SEM photographs of cross-sections of PCL foams formed under different saturated pressure. (Temperature = 40-C, saturation time =3 h, magnification = 150/50.) Top 14 MPa center 15 MPa bottom 16 MPa. [Pg.483]

Figure 4 Polarized photograph of cross-section of parts with micro-features surface. Process condition is standard. Figure 4 Polarized photograph of cross-section of parts with micro-features surface. Process condition is standard.

See other pages where Photograph of cross-section is mentioned: [Pg.195]    [Pg.339]    [Pg.502]    [Pg.350]    [Pg.74]    [Pg.58]    [Pg.83]   


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