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Published: 01 December 1998
Fig. 6 Crack growth comparison. Many commercial aluminum alloys show similar fatigue crack propagation rates in air, as indicated. More
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Published: 15 June 2019
Fig. 8 Comparison of 2 xxx and 7 xxx commercial aluminum alloys. (a) Notch toughness vs. yield strength. (b) Unit propagation energy vs. yield strength More
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Published: 15 June 2019
Fig. 45 Crack growth comparison. Many commercial aluminum alloys show similar fatigue crack propagation rates in air, as indicated above. L-T, longitudinal transverse; CNP, center-notch panel; DCB, double-cantilever beam; CT, compact tension. Source: Ref 90 More
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Published: 01 January 1996
Fig. 4 Comparison of 2XXX and 7XXX commercial aluminum alloys (a) Notch toughness vs. yield strength. (b) Unit propagation energy vs. yield strength More
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Published: 01 January 1996
Fig. 53 Crack growth comparison. Many commercial aluminum alloys show similar fatigue crack propagation rates in air, as indicated above. Source: Ref 90 More
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Published: 01 June 2024
Fig. 11 Optical micrographs of commercial aluminum alloys for cryogenic applications, showing variation in microstructures from the as-cast stage to the product fabrication stage. (a) AA2219 direct chill (DC) cast microstructure of large-sized ingot. (b) AA2219-T851 ring rolled to 2800 mm (110 More
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Published: 01 December 1998
Fig. 10 Structure of a commercial aluminum alloy 380 die casting. Etched in 0.5% HF; 500× More
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Published: 01 December 2004
Fig. 5 Typical examples of aluminum-magnesium commercial alloys. (a) Microstructure showing Al 3 Fe (gray) and Mg 2 Si (black) in α-aluminum solid-solution matrix (alloy type A518 with 7.6% Mg). Etchant: 0.5% HF. Original magnification 560×. (b) Microstructure showing ternary eutectic and α More
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Published: 01 January 1990
Fig. 5 Use of aluminum-lithium alloys in a commercial aircraft More
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003371
EISBN: 978-1-62708-195-5
... Abstract Metallic matrices are essential constituents for the fabrication of metal-matrix composites (MMCs). This article describes three different classes of aluminum alloys, namely, commercial aluminum alloys, low-density and high-modulus alloys, and high temperature alloys. It presents...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006482
EISBN: 978-1-62708-207-5
... Abstract Commercial aluminum alloys are classified based on how they are made and what they contain. This article describes the ANSI H35.1 designation system, which is widely used to classify wrought and cast aluminum alloys. The ANSI standard uses a four-digit numbering system to identify...
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Published: 30 November 2018
Fig. 3 Correlation between tensile yield, elongation, and magnesium content for some commercial aluminum alloys More
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Published: 01 January 1990
Fig. 6 Correlation between tensile yield, elongation, and magnesium content for some commercial aluminum alloys More
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Published: 01 December 1998
Fig. 3 Correlation between tensile yield, strength elongation, and magnesium content for some commercial aluminum alloys More
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Published: 30 November 2018
Fig. 2 Correlation between tensile yield strength, elongation, and magnesium content for some commercial aluminum alloys in the annealed temper. Source: Ref 9 More
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Published: 01 January 2006
Fig. 1 Correlation between tensile yield strength, elongation, and magnesium content for some commercial aluminum alloys in the annealed temper. Source: Ref 4 More
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in 355.0 and C355.0[1]: Al-Si-Cu High-Strength Casting Alloys > Properties and Selection of Aluminum Alloys
Published: 15 June 2019
Fig. 1 Growth and hardness curves for aluminum alloy 355.0 with various commercial tempers and aging at 175 °C (350 °F), permanent mold. Zero hour data is as-cast. Data at 0.3 h is after the l heat treatment. Data for aging at 175 °C (350 °F) is then given. Specimen: 28.575 diam × 305 mm More
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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) More
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Published: 01 June 2024
Fig. 13 Bright-field transmission electron micrographs of precipitate phases present in commercial aluminum alloys used in cryogenic propellant tanks of launch vehicles. (a) Distribution of θ′ phase. (b) Fine precipitation of T 1 and θ′ phases in the aluminum matrix, with the selected area More
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 June 2024
DOI: 10.31399/asm.hb.v12.a0007026
EISBN: 978-1-62708-387-4
... and mechanisms for the intended material, with fractographic examination of the failed part being a foremost piece in material failure analysis. For example, an early fractographic evaluation by Bhandarkar and Lisagor on a number of commercial aerospace aluminum alloys ( Ref 1 ) indicated that grain structure...