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Published: 01 December 2008
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Published: 01 January 1994
Fig. 1 Porosity in chromium plate as a function of plate thickness. Chromium deposited in low-temperature baths begins to crack at 75 μm (3000 μin.).
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Published: 01 January 1990
Fig. 26 Effect of plate thickness on notch toughness for aluminum semikilled steel (0.14C-1.25Mn-0.007S-0.020P-0.021Nb)
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Published: 31 October 2011
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Published: 31 October 2011
Fig. 8 Out-of-plane distortion (δ m ) as a function of plate thickness ( t ), span length ( l ), and the size of the fillet weld ( D f ) for steel and aluminum. Relation of l to a in graphs: a = l
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Published: 31 October 2011
Fig. 14 Thermal cycles calculated by Eq 9 for two distances. Plate thickness of 50 mm (2 in.); root gap of 24 mm (0.9 in.); I = 480 A; V = 35 V; v welding = 0.02 cm/s (0.008 in./s)
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Published: 01 January 1994
Fig. 3 Variations in hard chromium plate thickness for 74 loads, representing 110,000 parts of the same design plated over a period of 27 days of operation. Target thickness was 200 to 230 μm (8 to 9 mils) of hard chromium. Average thickness for the 74 loads was 215 μm (8.4 mils).
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Published: 01 January 1994
Fig. 5 Plate thickness deposited on the cross section of a cube-shape workpiece to show throwing power of cadmium relative to that of silver or copper in a cyanide bath. Open ends of the 100 mm (4 in.) cubes were pointed toward ball anodes during plating. Plating bath Thickness ratio
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Image
Published: 01 January 1994
Fig. 6 Variations in plate thickness obtained on a workpiece plated without the use of conforming anodes
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in Electromagnetic Acoustic Transducers for Nondestructive Evaluation
> Nondestructive Evaluation of Materials
Published: 01 August 2018
Fig. 11 In (a) through (d), T is the plate thickness, and λ = 2 D is the wavelength of the excitation force. (a) Normalized admittances for the n = 0 symmetric and antisymmetric Lamb modes and the SH 0 mode. (b) Normalized admittances for the n = 1 symmetric and antisymmetric Lamb
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Published: 01 December 1998
Fig. 41 Effect of plate thickness on notch toughness for aluminum semikilled steel (0.14C-1.25Mn-0.007S-0.020P-0.021Nb)
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in Procedure Development and Practice Considerations for Explosion Welding[1]
> Welding, Brazing, and Soldering
Published: 01 January 1993
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Published: 01 January 1993
Fig. 8 Out-of-plane distortion (δ m ) as a function of plate thickness ( t ), span length ( l ), and the size of the fillet weld ( D f ) for steel and aluminum. Relation of l to a in graphs: a = l
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Published: 01 February 2024
Fig. 10 Evolution of cooling rate with plate thickness to meet the hardness difference (ΔHV) conditions ΔHV = 0 and ΔHV = 20. C eq , carbon equivalent
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in Electroplated Coatings for Friction, Lubrication, and Wear Technology
> Friction, Lubrication, and Wear Technology
Published: 31 December 2017
Fig. 2 Nonuniform current distribution resulting in plating thickness variation. Adapted with permission from Ref 6
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Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006739
EISBN: 978-1-62708-210-5
... Abstract This datasheet provides information on composition limits, fabrication characteristics, processing effects on physical and mechanical properties, and application performance of thick plate and forging alloy 7085. It presents the specified minimum strength and fracture properties...
Abstract
This datasheet provides information on composition limits, fabrication characteristics, processing effects on physical and mechanical properties, and application performance of thick plate and forging alloy 7085. It presents the specified minimum strength and fracture properties for plate, die, and hand forgings. The datasheet provides a comparison of the strength, fracture toughness, and fatigue crack growth resistance of alloy 7085 plate with those of the legacy plate alloy 7050. It shows tensile yield and ultimate strength at elevated temperature for various temperatures and exposure times for 7085-T7452 die forgings.
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Published: 01 January 1996
Fig. 1 Operating stress map of a through-thickness crack in forged plate of Ti-6Al-4V with yield strength (σ y ) of 790 MPa (115 ksi) and K Ic of 83 MPa m (75 ksi in. )
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Published: 01 January 1996
Fig. 5 Operating stress map of Ti-6Al-4V plate with a through-thickness crack and net section yield lines for two plate widths ( W ). Same material as in Fig. 1 , σ y = 790 MPa (115 ksi) and K Ic = 83 MPa m (75 ksi in. )
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Published: 31 October 2011
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in Carbon and Low-Alloy Steel Plate
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
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