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Image
Published: 15 May 2022
Fig. 9 Tip scaling for profile extrusion die. (a) Tip-scaling process steps, progressing from left to right, in areas A, B, and C, circled. (b) Details of areas A, B, and C
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in Properties of Pure Metals
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 139 Scaling rate of zirconium at elevated temperature. Source: Ref 568
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Image
Published: 01 January 1994
Fig. 9 Oxidation of steels in air at the temperature at which scaling is less than 10 mg/cm 2 . Source: Ref 60
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in Principles of Superconductivity
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 8 Scaling law behavior of the critical current density ( J c ) for (a) several niobium-titanium alloys ( Ref 25 ) and (b) a Nb 3 Sn conductor ( Ref 26 ). In both cases, F p = J c B is plotted, scaled by the maximum value versus the reduced applied magnetic field, h = H a / H
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in Elevated-Temperature Properties of Ferritic Steels
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 28 Effect of temperature on metal loss from scaling for several carbon and alloy steels in air
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Published: 01 January 1990
Fig. 23 Scaling and growth of heavy section flake and compacted graphite cast irons at 600 °C (1110 °F). Source: Ref 9
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Published: 01 January 1990
Fig. 19 Relation of silicon and chromium contents to the scaling resistance of silicon-chromium irons. Indicated are the temperatures at which various irons can be used with very little or insignificant scaling in sulfur-free oxidizing atmospheres.
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Published: 01 June 2016
Fig. 5 Scaling rates of titanium and titanium alloys heated in air for 48 h. Source: Ref 2 , 3
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Published: 31 October 2011
Fig. 5 Comparison between the corrected scaling law and experiments with different materials and process parameters. Adapted from Ref 55
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Published: 01 December 1998
Fig. 1 Oxidation of steels in air at the temperature at which scaling is less than 10 mg/cm 2
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Published: 01 December 1998
Fig. 4 Relation of silicon and chromium contents to the scaling resistance of silicon-chromium irons. Temperatures indicated at which various irons can be used with very little or insignificant scaling in sulfur-free oxidizing atmospheres
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Published: 31 August 2017
Fig. 19 Scaling and growth of heavy-section flake and compacted graphite cast irons at 600 °C (1110 °F). CE, carbon equivalent. Source: Ref 11
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Published: 31 August 2017
Fig. 47 Scaling behavior of gray iron held in air at 900 °C (1650 °F). Original specimen was 10 mm (0.4 in.) in diameter and 30 mm (1.2 in.) in length. Source: Ref 76
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Published: 31 August 2017
Fig. 48 Effect of some alloying elements on scaling of lamellar graphite iron. (a) Gain in weight of irons listed in Table 19 after 200 h at temperature in air. Source: Ref 77 . (b) Effect of chromium on the gain in weight of a gray iron held at 800 °C (1470 °F). Source: Ref 78
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Published: 31 August 2017
Fig. 60 Relation of silicon and chromium contents to the scaling resistance of silicon-chromium irons. Indicated are the temperatures at which various irons can be used with very little or insignificant scaling in sulfur-free oxidizing atmospheres.
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Published: 12 September 2022
Fig. 7 (a) The scaling factor (σ 0 ) indicates the strength (98.5 MPa, or 14.3 ksi, flexural) with a failure probability of 0.63, while (b) the Weibull modulus of ~8.1 indicates a decent strength reliability in binder-jet-printed Ti-6Al-4V, which behaves as a brittle material due
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Published: 01 January 1997
Fig. 9 Oxidation of steels in air at the temperature at which scaling is less than 10 mg/cm 2 . Source: Ref 58
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Published: 01 January 2005
Fig. 3 Freeze-thaw cycles can cause scaling of concrete surfaces as shown on this pavement.
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Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003445
EISBN: 978-1-62708-195-5
... Abstract This article describes the role of the full-scale testing in assessing composite structural systems of aircraft and qualifying them for in-service use. The typical full-scale tests include static, durability, and damage tolerance. The article discusses the parameters to be considered...
Abstract
This article describes the role of the full-scale testing in assessing composite structural systems of aircraft and qualifying them for in-service use. The typical full-scale tests include static, durability, and damage tolerance. The article discusses the parameters to be considered when developing the basic requirements for the static test. These parameters consist of material considerations, moisture and temperature effects, structure size, load application alternatives, instrumentation requirements, test procedure considerations, ultimate load requirements, and test results correlation. The basic requirements common for durability and damage tolerance tests, including environmental effects and inspection requirements, are also discussed.
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005424
EISBN: 978-1-62708-196-2
... Abstract This article provides an explanation on how crystal plasticity is implemented within finite element formulations by the use of physical length scales: crystal scale and continuum scale. It provides theoretical formulations for kinematic framework for deforming crystals and polycrystals...
Abstract
This article provides an explanation on how crystal plasticity is implemented within finite element formulations by the use of physical length scales: crystal scale and continuum scale. It provides theoretical formulations for kinematic framework for deforming crystals and polycrystals, elastic and plastic behaviors of single crystals, refinements to the single-crystal constitutive, and crystal-scale finite-element. The article also presents examples that illustrate the capabilities of the formulations at the length scales.
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