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Published: 01 January 1996
Image
Effect of overaging on part through crack growth of aluminum alloy 7475 sub...
Available to PurchasePublished: 01 January 1996
Fig. 71 Effect of overaging on part through crack growth of aluminum alloy 7475 subject to 500 h block flight-by-flight fighter spectrum loading in sump tank water. Source: Ref 127
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Image
Published: 01 January 2005
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Corrosion-fatigue fracture in aluminum alloy 7475-T6 tested in a 3.5% NaCl ...
Available to PurchasePublished: 01 January 1987
Fig. 1058 Corrosion-fatigue fracture in aluminum alloy 7475-T6 tested in a 3.5% NaCl solution under a cyclic stress-intensity range (Δ K ) of 13 MPa m (12 ksi in. ) at 10 cps, showing contrasting features: ductile striations (unresolved) in smooth regions; brittle striations
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Crack resistance curves for aluminum alloy 7475 sheet. T-L, transverse-long...
Available to PurchasePublished: 15 June 2019
Fig. 22 Crack resistance curves for aluminum alloy 7475 sheet. T-L, transverse-longitudinal; L-T, longitudinal-transverse. Source: Ref 43
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Book Chapter
7475 Controlled-Toughness Sheet and Plate Alloy
Available to PurchaseSeries: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006747
EISBN: 978-1-62708-210-5
... Abstract Alloy 7475 is a controlled-toughness alloy for sheet and plate product forms. This datasheet provides information on key alloy metallurgy, processing effects on physical and mechanical properties, and fabrication characteristics of this 7xxx series alloy. aluminum alloy 7475...
Abstract
Alloy 7475 is a controlled-toughness alloy for sheet and plate product forms. This datasheet provides information on key alloy metallurgy, processing effects on physical and mechanical properties, and fabrication characteristics of this 7xxx series alloy.
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Examples of cavitation. (a) In aluminum (Al-7475) alloy. Courtesy of A.K. G...
Available to PurchasePublished: 01 January 2005
Fig. 27 Examples of cavitation. (a) In aluminum (Al-7475) alloy. Courtesy of A.K. Ghosh. (b) In titanium (Ti-6Al-4V) alloy. Source: Ref 37
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Book Chapter
7175 and 7475 High-Purity Versions of 7075
Available to PurchaseSeries: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006743
EISBN: 978-1-62708-210-5
... provides a fatigue life comparison of these alloys. aluminum alloy 7175 aluminum alloy 7475 ductility fatigue life physical properties Alloys 7175 and 7475 ( Table 1 ) are high-purity versions of 7075 to improve ductility in the transverse direction of thick products. The Zn/Mg ratio in 7175...
Abstract
Alloys 7175 and 7475 are high-purity versions of 7075 to improve ductility in the transverse direction of thick products. This datasheet provides information on key alloy metallurgy and processing effects on physical and mechanical properties of these 7xxx series alloys. It also provides a fatigue life comparison of these alloys.
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Published: 01 January 2006
Fig. 14 (a) Stress versus strain and (b) corresponding strain-rate sensitivity m for superplastic aluminum alloy 7475 in three different grain sizes. Tests were performed at 516 °C (960 °F), the optimal forming temperature for alloy 7475. Source: Ref 21
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Steps involved in thermal and mechanical processing to produce superplastic...
Available to PurchasePublished: 01 January 2006
Fig. 13 Steps involved in thermal and mechanical processing to produce superplastic aluminum alloy 7475. Source: Ref 30
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Aluminum alloys 2124 and 7475 are tougher versions of alloys 2024 and 7075....
Available to PurchasePublished: 01 January 1996
Fig. 7 Aluminum alloys 2124 and 7475 are tougher versions of alloys 2024 and 7075. High-purity metal (low iron and silicon) and special processing techniques are needed to optimize toughness in these materials. Source: Ref 14
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Fracture toughness comparisons of aluminum alloys 2024, 2124, 7075 and 7475...
Available to PurchasePublished: 01 January 1996
Fig. 12 Fracture toughness comparisons of aluminum alloys 2024, 2124, 7075 and 7475. Source: Ref 15
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Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006457
EISBN: 978-1-62708-210-5
... copper, chromium, silicon, and iron from commercial alloys. Consequently, an often-used approach to improve the toughness of high-strength aluminum alloys has been the reduction of iron and silicon levels. The development of improved alloys such as 7475, 7050, and 2124 has hinged, in large part, upon...
Abstract
This article discusses the concepts underlying linear elastic fracture mechanics and elastic-plastic fracture mechanics as well as their importance in characterizing the fracture behavior of the high-strength aluminum alloys. It describes the three methods used for analyzing elastic-plastic fracture, namely R-curve concept, J-integral concept, and crack tip opening displacement method. The article considers the primary measures used to assess the toughness of aluminum alloy castings and wrought alloys: notch toughness, tear resistance, and plane-strain fracture toughness.
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0009013
EISBN: 978-1-62708-185-6
.... Examples of hermomechanical Testing: Design, Experiment, and Analysis Four examples illustrate how the various considerations in testing are successfully used to solve practical thermomechanical processing problems. Example 1: Superplastic Forming of Aluminum Alloy 7475 This first example...
Abstract
Thermomechanical are used to gain insight into the causes of problems that arise during a given thermomechanical process. This article provides examples to demonstrate how significant the parameters were selected for specific tests. It examines the types of problems that can occur during a thermomechanical process. The article provides information on the thermophysical properties, which include specific heat, coefficient of thermal expansion, thermal conductivity/diffusivity, and density. It concludes with examples that illustrate how the various considerations in testing are successfully used to solve practical thermomechanical processing problems.
Book Chapter
Selecting Aluminum Alloys to Resist Failure by Fracture Mechanisms
Available to PurchaseBook: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002406
EISBN: 978-1-62708-193-1
... of one high-toughness aluminum alloy (7475-T7351) are shown in Table 4 . Typical room-temperature yield strength and plane-strain fracture toughness values for several high-strength aluminum alloys Table 3 Typical room-temperature yield strength and plane-strain fracture toughness values...
Abstract
This article provides an overview of fatigue and fracture resistance of aluminum alloys. It discusses the characteristics of aluminum alloy classes and the fracture mechanics of aluminum alloys. The article tabulates relative stress-corrosion cracking ratings for high-strength wrought aluminum products. It analyzes the selection of various alloys for stress-corrosion cracking resistance, including aluminum-lithium alloys, copper-free 7XXX alloys, and casting alloys. The article presents a list of typical tensile properties and fatigue limit of aluminum alloys. It also describes the effects of composition, microstructure, thermal treatments, and processing in fatigue crack growth of aluminum alloys.
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Fracture toughness comparisons of aluminum alloys 2024, 2124, 7075, and 747...
Available to PurchasePublished: 15 June 2019
Fig. 17 Fracture toughness comparisons of aluminum alloys 2024, 2124, 7075, and 7475. Aluminum alloys 2124 and 7475 are tougher versions of alloys 2024 and 7075. High-purity metal (low iron and silicon) and special processing techniques are needed to optimize toughness in these materials
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Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005141
EISBN: 978-1-62708-186-3
... Abstract This article discusses the general formability considerations of aluminum alloys. To conduct a complete analysis of a formed part, the required mechanical properties, as determined by several standard tests, must be considered. The article describes tension testing and other tests...
Abstract
This article discusses the general formability considerations of aluminum alloys. To conduct a complete analysis of a formed part, the required mechanical properties, as determined by several standard tests, must be considered. The article describes tension testing and other tests designed to simulate various production forming processes, including cup tests and bend tests, which help in determining these properties. It provides information on the equipment and tools, which are used in the forming of aluminum alloys. The article presents a list of lubricants that are most widely used in the forming. It also analyzes the various forming processes of aluminum alloys. The processes include blanking and piercing, bending, press-brake forming, contour roll forming, deep drawing, spinning, stretch forming, rubber-pad forming, warm forming, superplastic forming, explosive forming, electrohydraulic forming, electromagnetic forming, hydraulic forming, shot peening, and drop hammer forming.
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(a) The decrease in fracture strain with increase of volume percent of micr...
Available to PurchasePublished: 01 January 1996
Fig. 10 (a) The decrease in fracture strain with increase of volume percent of micron-size intermetallic particles for a super-purity aluminum matrix and an Al-4Mg matrix. (b) A comparison of high-purity 7050 aluminum sheet, 7475 sheet, and a 7 xxx -series aluminum alloy. Tear strength
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Variations in fatigue striation spacing. (a) Spectrum-loaded fatigue fractu...
Available to PurchasePublished: 01 January 1987
Fig. 25 Variations in fatigue striation spacing. (a) Spectrum-loaded fatigue fracture in a 7475-T7651 aluminum alloy test coupon showing an increase in striation spacing due to higher alternating stress. (b) Local variation in fatigue striation spacing in a spectrum-loaded 7050-T7651 aluminum
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Image
Published: 01 January 1996
Fig. 10 Critical stress intensity factor, K c , vs. tensile yield strength for 1.0 to 4.7 mm (0.040 to 0.188 in.) aluminum alloy sheet. Improved alloy 7475 is compared to other commercial alloys. Source: Ref 10
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