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aluminum alloy plates

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Published: 01 August 2005
Fig. 2.65 Tensile stress-strain curve for a 2024-T351 aluminum alloy plate. Source: Ref 2.39 More
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Published: 01 August 1999
Fig. 5 Comparison of residual stresses in a thick, constant cross-section of 7075-T6 aluminum alloy plate before and after stress relief. (a) High residual stresses in the solution-treated and quenched alloy. (b) Reduction in stresses after stretching 2%. Source: Ref 10 More
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Published: 01 January 2017
Fig. 8.7 Comparison of residual stresses in a thick, constant cross-section 7075-T6 aluminum alloy plate before and after stress relief. (a) High residual stresses in the solution-treated and quenched alloy. (b) Reduction in stresses after stretching 2%. Source: Ref 8.18 More
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Published: 01 July 2009
Fig. 14.7 AlBeMet aluminum-beryllium alloy sheet and plate manufacturing sequence More
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Published: 01 August 1999
Fig. 33 Corrosion fatigue behavior of aluminum alloy 7079-T651 plate (S-L orientation). Temperature: 23 °C (73 °F); frequency: 4 cycles/s; stress ratio; R = 0. (a) Effect of stress intensity range on crack growth rate. K ICFC and a range of K ISCC are indicated at the bottom. (b More
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Published: 01 August 2005
Fig. 3.9 Tube-to-plate joint in aluminum engineering alloy components, torch brazed in air using a low-melting-point aluminum-base filler metal and commercially available flux More
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Published: 01 August 2005
Fig. 4.17 K IC versus F ty plot showing the improvement of K IC values for 7475 aluminum alloy plate (L-T orientation), accomplished by reducing iron and silicon contents, optimizing dispersoids, altering precipitates, and controlling quenching rate and grain size. Source: Ref 4.22 More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870135
EISBN: 978-1-62708-299-0
... of pitting for aluminum alloy plate specimens after immersion in seawater Table 8 Average weight loss and maximum depth of pitting for aluminum alloy plate specimens after immersion in seawater Specimens were 6.35 × 305 mm (0.250 × 12 × 12 in.) and weighed approximately 1.6 kg (3.5 lb). Test...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540397
EISBN: 978-1-62708-309-6
...: Ref A7.11 A7.3 Aluminum-Lithium Alloys Sheet and plate mechanical properties data for the low-density 8090 and 2090 Al-Li alloys are presented in Table A7.5 . Table A7.6 lists the test results for extrusions. Fatigue and fatigue crack growth rate data for the 8090-TU51 extrusion are shown...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870099
EISBN: 978-1-62708-299-0
... tensile stress is necessary to initiate and propagate this type of corrosion. Fig. 5 Comparison of residual stresses in a thick, constant cross-section of 7075-T6 aluminum alloy plate before and after stress relief. (a) High residual stresses in the solution-treated and quenched alloy. (b...
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340117
EISBN: 978-1-62708-427-7
... ). These thinner products are predominantly produced at widths of 2500 mm (100 in.) or less due to limitations of continuous coilers. Continuous hot mills cannot easily coil aluminum, especially hard 5 xxx alloys, at greater than approximately 12 mm thickness. Fig. 6.8 Aluminum plate rolling Plate...
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340245
EISBN: 978-1-62708-427-7
... 7199 2014 0.10 0.12 1.4–2.1 0.04 1.6–2.3 0.04 7.4–8.4 0.06 0.05–0.15 Plate: ribs, spars, wings, fuselage Commonly used 2<italic>xxx</italic> aluminum alloys for aircraft structures Table 11.4 Commonly used 2 xxx aluminum alloys for aircraft structures Alloy Year Si Fe Cu...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140175
EISBN: 978-1-62708-335-5
... 16 in. thick plate Fig. D2.31 Growth curves for aluminum alloy 380.0-F, die cast. Specimen: 3 16 in. thick plate Fig. D2.32 Growth curves for aluminum alloy 384.0-F, die cast. Specimen: 5 16 in. thick plate Fig. D2.33 Growth curves...
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340325
EISBN: 978-1-62708-427-7
... corrosion. (a) 5083 plate microstructure in sensitized condition. (b) Stress-corrosion cracking (SCC) adjacent to welds in a ship structure Since 2003, the Aluminum Association has had a temper specification to be applied for 5 xxx alloys used in shipbuilding. The need for the new spec arose when...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2015
DOI: 10.31399/asm.tb.cpi2.t55030169
EISBN: 978-1-62708-282-2
... contain magnesium and/or manganese. The alloys in this series are strengthened by thermal processing. These alloys attain high strengths and are used in sheet, plate, and extruded forms, primarily in aerospace applications. Copper in aluminum alloys generally decreases the resistance to general corrosion...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870001
EISBN: 978-1-62708-299-0
... Abstract Aluminum is the second most widely used metal in the world. It is readily available, offers a wide range of properties, and can be shaped, coated, and joined using a variety of methods. This chapter discusses some of the key attributes of wrought and cast aluminum alloys...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870191
EISBN: 978-1-62708-299-0
...) as a result of soil accumulation. Finishes are applied to aluminum alloys for aesthetic reasons and to provide protection against corrosion. These finishes include nonfinished (bare) aluminum, anodized aluminum, conversion coatings, painted aluminum, porcelain finishes, and plated finishes. In retarding...
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340413
EISBN: 978-1-62708-427-7
... and steel sheet was commonly used. When that practice ended, it was evident that the car tags would need to last much longer, up to the life of the vehicle. As a result, aluminum license plates are widely used today, produced from alloys such as 1100 or 3003 in H14-H24 tempers. The choice of temper...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2008
DOI: 10.31399/asm.tb.emea.t52240487
EISBN: 978-1-62708-251-8
... properties of select wrought heat treatable aluminum alloys Alloy Temper Product form Tensile strength Yield strength Elongation in 50 mm (2 in.), % MPa ksi MPa ksi 2008 T4 Sheet 250 36 125 18 28 T6 Sheet 300 44 240 35 13 2014 T6, T651 Plate, forging 485 70 415...
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340375
EISBN: 978-1-62708-427-7
... Abstract Aluminum alloy products offer architectural and building solutions that exploit the benefits inherent in this metal: light weight, excellent durability, low maintenance, and thermal management opportunities. This chapter discusses the major applications for aluminum building products...