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Laminations

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Published: 01 November 2013
Fig. 23 Laminations in rolled steel sheet resulting from insufficient cropping of the pipe from the top of a conventionally cast ingot. Courtesy of V. Demski, Teledyne Rodney Metals. Source: Ref 14 More
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Published: 01 June 1988
Fig. 9.9 High-permeability laminations used to divert the magnetic flux field and thus prevent stray heating within a stainless steel vessel More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2008
DOI: 10.31399/asm.tb.emea.t52240607
EISBN: 978-1-62708-251-8
..., and performance-cost tradeoffs of common MMCs, including aluminum-matrix composites, titanium-matrix composites, and fiber-metal laminates. It also explains how fiber-reinforced composites and laminates are made, describing both continuous and discontinuous fiber matrix production processes. metal-matrix...
Book Chapter

By M. B. Kasen
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 1983
DOI: 10.31399/asm.tb.mlt.t62860413
EISBN: 978-1-62708-348-5
...Industrial high-pressure laminates of primary Interest for cryogenic applications. Table 12.1 Industrial high-pressure laminates of primary Interest for cryogenic applications. Commercial Standard MIL-P and LP Designation Description NEMA/ASTM LE MIL-P-15035, type FBE Cellulose...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060183
EISBN: 978-1-62708-355-3
... bevel angle; W width. Note: the gage length is commonly 125 to 150 mm (5 to 6 in.). Fig. 4 Typical tension failure of multidirectional laminate using a tabbed coupon Fig. 5 Schematic of typical ASTM D 638 test specimen geometry. W , width; W c , width at center; WO , width...
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Published: 01 November 2019
Figure 11 (a) The current path extends through the laminate via the expected path but diverges along an abnormal path as soon as it reaches the chip. (b) The current path extends into the module after the abnormally through a module test structure. More
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Published: 01 November 2019
Figure 13 SAM images of a test die on an interposer and laminate. (a) Diagram of structure scanned (b) Reflected signal scan at die to interposer interface, (c) Reflected signal scan at interposer to laminate interface showing a large area of delamination (d) Transmitted scan signal of entire More
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Published: 01 November 2019
Figure 15 (a) Image focused on laminate (b) Image focused on interposer (c) Image focused on die (d) Compilation of 100 images reconstructed to show laminate, interposer, and die in focus More
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Published: 01 November 2019
Figure 16 (a) Image focused on laminate (b) Image focused on defect at corner (c) Image focused on interposer (d) Compilation of 100 images reconstructed to show laminate, corner defect, and die in focus More
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Published: 01 November 2019
Figure 19 3D tomography of the solder bumps connecting the laminate to the interposer along with micropillars connecting the HBM modules to each other and to the interposer More
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Published: 01 March 2006
Fig. 12.53 Two 8-ply laminates. (a) Symmetric. (b) Nonsymmetric More
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Published: 01 March 2006
Fig. 12.54 Defining plies, orientation, loads, and stresses and strains in laminates of continuous fiber-reinforced matrix material. Source: Ref 12.24 More
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Published: 01 June 1983
Figure 12.3 The conventional notation for uniaxial (a) and crossply (b) laminates. The crossply laminate is designated [0/±45/0] T . More
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Published: 01 June 1983
Figure 12.20 Temperature dependence of thermal conductivity of uniaxial laminates. L = longitudinal, T = transverse. Transverse conductivity of the aramid laminate assumed from fabric-reinforced data. Vol.% = fiber volumefraction. Refs.: (1) Hust and Arvidson (1978) ; (2) Dahlerup-Petersen More
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Published: 01 June 1983
Figure 12.36 Tensile grip assembly for testing laminates at cryogenic temperature. More
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Published: 01 June 1983
Figure 12.37 Grip system for tensile fatigue testing of laminates at cryogenic temperatures. Example is a waisted specimen used with [0/±45/0] S , 140- μ m (5.6-mil) boron-epoxy. More
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Published: 01 June 1983
Figure 12.39 Specimen configuration used for compression testing of laminates at cryogenic temperature; (a) square specimen; (b) round specimen. More
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Published: 01 November 2010
Fig. 2.3 Carbon fiber composite laminate labeled for sectioning using a silver ink felt-tip permanent marker. This sample with the corresponding section map was originally sent for nondestructive inspection. More
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Published: 01 November 2010
Fig. 8.2 Laminate made with unidirectional carbon fiber prepreg and woven carbon fabric prepreg plies. Voids are shown in the woven fabric area at the bottom of the composite part that was against the tool surface during cure. Bright-field illumination, 65 mm macrophotograph More
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Published: 01 November 2010
Fig. 9.1 Microcracks in a carbon fiber composite laminate due to thermal cycling. (a) Resin-rich region in the composite. Slightly uncrossed polarized light, 10× objective. (b) Resin-rich region containing a large void. Slightly uncrossed polarized light, 10× objective More