Skip Nav Destination
Close Modal
Search Results for
7075-T7351
Update search
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
NARROW
Format
Topics
Book Series
Date
Availability
1-20 of 49 Search Results for
7075-T7351
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Image
Published: 01 December 2009
Fig. 8 Crack growth in 7075-T7351 aluminum alloy subject to spectrum loading. (a) Crack-growth comparison between model and experiment. LCD is a linear-cumulative damage model, and α = 1.8 is a constant constraint model. (b) Wing gust and maneuver loading spectrum. Source: Ref 23
More
Image
Published: 01 January 2003
Fig. 44 Crack depth and stress intensity versus time curves for double-beam specimens of aluminum alloys 7075-T651, 7079-T651, and 7075-T7351 having nearly identical deflections and starting crack depths. Specimens with S-L orientation (see Fig. 28 ) measuring 25 × 25 × 127 mm (1 × 1 × 5
More
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006606
EISBN: 978-1-62708-210-5
...-T86 plate static properties Property Direction 2099-T86 (AMS 4458) 7075-T7351 (AMS 4078) 7050-T7451 (AMS 4050) Thickness, mm (in.) 13–25 (0.5–50) 25–50 (1.0–2.0) 6–50 (0.250–2.0) Tensile strength F tu , MPa (ksi) L 490 (71) 476 (69) 510 (74) L-T 496 (72) 476 (69) 510 (74...
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006607
EISBN: 978-1-62708-210-5
... and 7075-T7351 plate Table 5 Nominal elevated-temperature yield strength of 2124-T851 and 7075-T7351 plate Alloy-temper Exposure time, h Temperature, °C (°F) Yield strength, MPa (ksi) 2124-T851 10 24 (75) 440 (64) 100 (212) 420 (61) 150 (300) 395 (57) 205 (400) 310 (45...
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006737
EISBN: 978-1-62708-210-5
... (7075): forgings and forging stock (7049 and 7075) T7351 Solution heat treated, stretched a controlled amount (product dependent) for stress relief, and artificially overaged to achieve best corrosion resistance with a greater reduction in strength than T74 (no further straightening after stretching...
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006594
EISBN: 978-1-62708-210-5
... tolerance 7075-T76 7075-T73 2214-T6 2014-T6 2219-T87 2098-T8 7010-T7651 2214-T651 2014-T651 7075-T7351 7475-T7351 7050-T7651 2124-T851 2129-T852 2099-T86 7050-T74 7050-T7452 7075-T73 7075-T7352 2014-T652 2024-T852 2040-T6 2040-T852 … 2219-T851 2024-T8511 2014-T6511 7075-T73511 7055-T74511 7136-T74511...
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
... (22) 7075-T6 Extrusion 13–20 (0.5–0.75) 32 (29) 23 (21) 21 (19) 7075-T651 Plate 13–50 (0.5–2.0) 29 (26) 24 (22) 20 (18) 7075-T7351 Plate 13–50 (0.5–2.0) 33 (30) 33 (30) 25 (23) 7075-T7651 Plate 13–50 (0.5–2.0) 30 (27) 25 (23) 21 (19) 7475-T7351 Plate 30–100 (1.3...
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.
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006622
EISBN: 978-1-62708-210-5
... and forging stock (7049 and 7075) T7351 Solution heat treated, stretched a controlled amount (product dependent) for stress relief, and artificially overaged to achieve best corrosion resistance with a greater reduction in strength than T74 (no further straightening after stretching) 7075, alclad 7075...
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
... 2024 and 7075, which have been used for components that do not require a high level of fracture toughness. Typical data for a lot of one high-toughness aluminum alloy (7475-T7351) are shown in Table 2 . Typical strength and fracture toughness properties of several high-strength aluminum products...
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.
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006747
EISBN: 978-1-62708-210-5
... T7351 AMS 4202C Bare sheet T61 AMS 4084C T761 AMS 4085B Alclad sheet T61 AMS 4207A T761 AMS 4100A Physical and mechanical properties are given in Tables 2 and 3 , respectively. Tensile property minimums are given in Tables 4 and 5 . Unlike alloy 7075 (which does...
Book Chapter
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006531
EISBN: 978-1-62708-207-5
... (7075); rolled or cold-finished rod, bar, and wire (7075); rivets (7075); forgings and forging stock (7049 and 7075) T7351 Solution heat treated, stretched a controlled amount (product dependent) for stress relief, and artificially overaged to achieve best corrosion resistance with a greater...
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006743
EISBN: 978-1-62708-210-5
... 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...
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.
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005419
EISBN: 978-1-62708-196-2
... but incorporated by linearly transitioning from the plane-strain to plain-stress growth modes dependent on the crack-growth rates. Figure 8 shows crack growth in aluminum alloy 7075-T7351 subject to a wing gust and maneuver load spectrum ( Ref 23 ). A comparison of predictions between the experimental results...
Abstract
Understanding fatigue crack growth is critical for the safe operation of many structural components. This article reviews the standard fracture mechanics and methods to determine the crack growth rate for a material and loading condition experimentally. It also addresses the two most important aspects of crack-growth modeling: loading environment and crack geometry.
Book: 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
... T7651 470 68 30 27 24 22 20 18 7075 T7351 435 63 32 29 29 26 21 19 7475 T651 495 72 43 39 37 34 32 29 7475 T7651 460 67 47 43 39 35 31 28 7475 T7351 430 62 53 48 42 38 35 32 Die forgings 7050 T736 455 66 36 (b) 33 (b) 25 (c) 23 (c...
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.
Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003126
EISBN: 978-1-62708-199-3
...) … … … … 6262-T9 510 (74) 427 (62) 415 (60) 400 (58) 365 (53) 262 (38) 103 (15) 59 (8.5) 32 (4.6) 21 (3) 7075-T6, T651 703 (102) 620 (90) 593 (86) 572 (83) 483 (70) 215 (31) 110 (16) 75 (11) 55 (8) 40 (6) 7075-T73, T7351 635 (92) 545 (79) 525 (76) 503 (73) 435 (63) 215 (31) 110...
Abstract
This article is a comprehensive collection of property data for wrought aluminum and aluminum alloys. Data are provided for the physical properties and mechanical properties of wrought aluminum and aluminum alloys. The listing also includes values that indicate the effect of temperatures on tensile strength, yield strength, and elongation, and the mechanical properly limits for aluminum alloy die forgings, non-heat-treatable and heat-treatable aluminum alloy sheets and plates, and non-heat-treatable aluminum alloy extruded wires, rods, bars, and shapes.
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006544
EISBN: 978-1-62708-210-5
... properties of aluminum alloy plate, hand forgings, and extrusions Table 1 Minimum tensile properties of aluminum alloy plate, hand forgings, and extrusions Direction Plate (a) Hand forgings (b) Extrusions (c) 7075-T651 7075-T7351 7075-T6 7075-T7351 7075-T6511 7075-T7351 Tensile...
Abstract
Understanding the mechanical properties of aluminum alloys is useful for the designer for choosing the best alloy and establishing appropriate allowable stress values, and for the aluminum producer to control the fabrication processes. This article discusses the nature and significance of mechanical property data and of stress-strain curves detailing the effects of mechanical properties on the design and selection of aluminum alloys. The properties include tensile, compressive, shear, bearing, creep and creep-rupture, fatigue, and fracture resistance properties.
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001059
EISBN: 978-1-62708-162-7
... and trim sections T5 A A B C A A A A NA T6 A A C C A A A A 7005 T53 B B C A B B B B B Heavy-duty structures requiring good corrosion resistance, trucks, trailers, dump bodies 7049 T73, T7351, T7352 C B D B D C B D D Aircraft and other structures T76...
Abstract
Aluminum mill products are those that have been subjected to plastic deformation by hot- and cold-working mill processes such as rolling, extruding, and drawing, either singly or in combination. Microstructural changes associated with the working and with any accompanying thermal treatments are used to control certain properties and characteristics of the worked, or wrought, product or alloy. This article discusses the designation system, classification, product forms, corrosion and fabrication characteristics, and applications of wrought aluminum alloys. Commercial wrought aluminum products are divided into flat-rolled products (sheet, plate, and foil); rod, bar, and wire; tubular products; shapes; and forgings. The article discusses factors affecting the strengthening mechanisms, fracture toughness, and physical properties of aluminum alloys, in addition to the effects of alloying on the physical and mechanical properties. Important alloying elements and impurities are listed alphabetically as a concise review of major effects.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006289
EISBN: 978-1-62708-169-6
... 7050-T736 and T73651 40.50 7072 60.00–60.10 7072-O 60.00 7075-F 44.50–47.80 7075-T6 31.40–34.80 7075-T6 32.00 7075-W 27.00–37.00 7075-T6, T62, T651, and T652 33.00 7075-T76 and T7651 38.50 7075-T73, T7351, and T7352 40.00 7076 35.00 7175-O 46.00 7175-T66...
Abstract
Heat treatment of aluminum alloys is assessed by various quality-assurance methods that include metallographic examination, hardness measurements, mechanical property tests, corrosion-resistance tests, and electrical conductivity testing. The use of hardness measurements in the quality assurance of heat treated aluminum products is effectively used in conjunction with the measurement of surface electrical conductivity. This article provides a detailed discussion of the error sources in eddy-current conductivity measurements. It also presents useful information on the variation of electrical conductivity of alloy 2024 samples as a function of aging time at different isothermal holding temperatures.
Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003125
EISBN: 978-1-62708-199-3
... … … 7050 … T7451 (c) , T7651 … … … … T73510, T73511, T74510 (c) , T74511 (c) , T76510, T76511 H13 … H13 T7 T74 (c) , T7452 (c) , F … … 7072 … … … … … … … … … … … … … O, H14, H18, H19, H23, H24, H241, H25, H111, H113, H211 7075 T6, T73, T76 O, T651, T7351, T7651 O, T6...
Abstract
This article discusses the classification, characteristics and temper designations of wrought aluminum alloys. Wrought aluminum products are available as flat-rolled products such as sheets, plates, and foils; rods, bars, and wires; tubular products such as tubes and pipes; extruded shapes; forgings; and impacts. The article provides information on product economics, design and selection, including product dimension and dimension tolerances, and design and use of wrought product capabilities. Finally, it tabulates the specifications and standards for aluminum mill products.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006288
EISBN: 978-1-62708-169-6
..., bar, and wire, (7075); rivets (7075): forgings and forging stock (7049 and 7075) T7351 Solution heat treated, stretched a controlled amount (product dependent) for stress relief, and artificially overaged to achieve best corrosion resistance with a greater reduction in strength than T74...
Abstract
This article focuses on the aging characteristics of solution and precipitation heat treated aluminum alloy systems and their corresponding types. It includes information on aluminum-copper systems, aluminum-copper-magnesium systems, aluminum-magnesium-silicon systems, aluminum-zinc-magnesium systems, aluminum-zinc-magnesium-copper systems, and aluminum-lithium alloys.