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Search Results for aluminum alloy plates
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Image
Published: 01 January 2002
Fig. 20 Fatigue-fracture zones in aluminum alloy 7075-T6 plates. (a) Fatigue crack that grew as a flat-face fracture with a shallow convex crack front. (b) Change in orientation of fatigue fracture from plane strain (arrow A) to plane stress (arrow B).
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Published: 15 January 2021
Fig. 57 Liquid metal embrittlement in two aluminum alloy 2024-T4 plates that were wetted with liquid mercury and then loaded to fracture in tension. Fracture occurred rapidly at a stress well below the nominal yield strength of the plates. Visible on each fracture surface is a flat, mercury
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Published: 15 January 2021
Fig. 29 Fatigue fracture zones in aluminum alloy 7075-T6 plates. (a) Fatigue crack that grew as a flat-face fracture with a shallow convex crack front. (b) Change in orientation of fatigue fracture from plane strain (arrow A) to plane stress (arrow B)
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Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006744
EISBN: 978-1-62708-210-5
... Abstract This datasheet provides information on composition limits for aluminum alloy 7255, with emphasis on the minimum static properties of aluminum alloy 7255 plate and fracture toughness of aluminum alloy 7255-T7751. Fatigue crack growth resistance of alloy 7255 plate is compared with those...
Abstract
This datasheet provides information on composition limits for aluminum alloy 7255, with emphasis on the minimum static properties of aluminum alloy 7255 plate and fracture toughness of aluminum alloy 7255-T7751. Fatigue crack growth resistance of alloy 7255 plate is compared with those of legacy alloy 7055 plate.
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006740
EISBN: 978-1-62708-210-5
... effects on mechanical properties of alloy 7097-T7651 plate. aluminum alloy 7097 aluminum alloy plates aluminum-magnesium-zinc-copper-zirconium alloys corrosion resistance fracture toughness mechanical strength thick structural applications Alloy 7097 ( Table 1 ) from Kaiser Aluminum...
Abstract
Alloy 7097 is a quench insensitive Al-Mg-Zn-Cu-Zr alloy engineered for the most advantageous combination of strength, corrosion resistance, and fracture toughness in thick structural applications. This datasheet provides information on key alloy metallurgy of alloy 7097 and processing effects on mechanical properties of alloy 7097-T7651 plate.
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006731
EISBN: 978-1-62708-210-5
... of aluminum alloys 7040 and 7140 and processing effects on mechanical properties of aluminum alloy 7040-T7651 high-strength plate. aluminum alloys 7040 aluminum alloys 7140 chemical composition fabrication characteristics high-strength plate hot-worked products mechanical properties...
Abstract
Alloy 7040 is a variation of 7050, where Zr additions prevent recrystallization of hot-worked products during solution heat treatment without the quench sensitivity from additions of Cr. This datasheet provides information on composition limits and fabrication characteristics of aluminum alloys 7040 and 7140 and processing effects on mechanical properties of aluminum alloy 7040-T7651 high-strength plate.
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006741
EISBN: 978-1-62708-210-5
... for 100-mm (4-in.) thick plate product. Source: Ref 3 Fig. 2 T7651 S / N fatigue curve. Tested using open-hole test specimen according to ASTM E 466. Typical L-T orientation curve shown for 100-mm (4-in.) gage specimen. Source: Ref 4 References References 1. “ Aluminum Alloy...
Abstract
The aluminum alloy 7099 is a Kaiser aluminum high-strength Al-Mg-Zn-Cu alloy with zirconium that offers a less quench-sensitive alloy for properties in thicker sections for airframe structures such as wing ribs, spars, and skins, as well as fuselage frames and floor beams. This datasheet provides information on key alloy metallurgy and processing effects on mechanical properties of this 7xxx series alloy.
Image
Published: 01 June 2024
Fig. 11 SEM and deep-focus optical fractography examples of changes in fatigue fracture surface orientations due to load history variations. (a) Changes in overall fracture planes for AA7075-T6 aluminum alloy thin plate when a simple flight-by-flight variable-amplitude load sequence
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Image
Published: 15 June 2019
Fig. 12 (a) Crack propagation rates in stress-corrosion tests using precracked thick, double-cantilever beam specimens of high-strength 2 xxx -series aluminum alloy plate, transverse-long (short-longitudinal) orientation. Specimens were wet twice a day with an aqueous solution of 3.5% NaCl, 23
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Image
Published: 01 January 2005
Fig. 10 (a) Crack propagation rates in stress-corrosion tests using precracked thick, double-cantilever beam specimens of high-strength 2 xxx -series aluminum alloy plate, TL (SL) orientation. Specimens were wet twice a day with an aqueous solution of 3.5% NaCl, 23 °C (73 °F). (b) Crack
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Image
Published: 15 June 2019
Fig. 16 Unit crack propagation energies (UPEs). (a) Commercial 7 xxx aluminum alloy plate in peak strength and overaged tempers. (b) Effects of dispersoid type on toughness of 75 mm (3 in.) 7075 plate. Source: Ref 22
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Image
Published: 01 January 1996
Fig. 6 Unit crack propagation energies (UPE), (a) commercial 7XXX aluminum alloy plate in peak strength and overaged tempers (Source: Ref 10 ) and (b) effects of dispersoid type on toughness of 75 mm (3 in.) 7075 plate (Source: J. Staley in ASTM STP 605)
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in Aluminum Foundry Products
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 13 Comparison of (a) notch yield ratio and (b) unit propagation energy versus yield strength for various aluminum alloy premium-quality castings and wrought aluminum alloy plate. 1, XA201.0-T7; 2, 249.0-T7; 3, 224.0-T7; 4, C355.0-T6; 5, 354.0-T6; 6, A356.0-T6; 7, 356.0-T6; 8, A357.0-T6
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Image
Published: 15 June 2019
Fig. 11 Comparison of residual stresses in a thick, constant cross-sectional 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 65
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Image
Published: 01 January 2005
Fig. 13 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 68
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Image
Published: 01 January 1996
Fig. 9 Fracture toughness vs. yield strength for high-strength aluminum alloy plate (L-T orientation)
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Published: 15 June 2019
Fig. 20 Fracture toughness vs. yield strength for high-strength aluminum alloy plate (longitudinal-transverse orientation). Source: Ref 43
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Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006726
EISBN: 978-1-62708-210-5
... hardening tensile strength wrought heat treatable aluminum alloys COMMERCIAL 7 XXX SERIES ALLOYS are capable of being heat treated to exceptionally high strength levels (>600 MPa, or 87 ksi, yield strength). They are commonly produced in the form of sheet, plate, extrusions, rod, bar...
Abstract
Wrought heat treatable 7xxx alloys are more responsive to precipitation hardening than the 2xxx series alloys and can achieve higher strength levels, approaching tensile strengths of 690 MPa (100 ksi). This article provides an overview of key metallurgy, properties, and applications of the 7xxx aluminum alloy. It also illustrates the natural aging characteristics of 7050 aluminum sheet alloys at room temperature and relationships among commonly used alloys in the 7xxx series.
Image
Published: 30 November 2018
Fig. 26 Comparison of fatigue life for arc-welded and friction-stir-welded (FSW) joints in 6082-T6 aluminum alloy plates. MIG, metal inert gas; TIG, tungsten inert gas. Source: Ref 27
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Image
Published: 01 June 2024
Fig. 7 Optical and SEM images of constant-amplitude marker bands on the fatigue fracture surface of an AA7075-T651 aluminum alloy plate specimen. The marker bands were obtained by grouping 2204 cycles extracted from the BASIC spectrum and placing the group just before the peak load
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