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Published: 15 June 2019
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006617
EISBN: 978-1-62708-210-5
... properties, and applications of this alloy. Figures provide comparisons of plane stress R-curves of 2624 with 2024-T351 and 2324-T39 and fatigue crack growth resistance of 2624 with 2024-T351 and 2324-T39. alloy composition aluminum alloy 2624 damage tolerant plate fatigue crack growth resistance...
Abstract
Alloy 2624 was developed by Alcoa as a plate product to replace alloy 2024 and 2324 in applications requiring moderate or high strength and the highest levels of damage tolerance. This datasheet provides information on composition limits, processing effects on physical and mechanical properties, and applications of this alloy. Figures provide comparisons of plane stress R-curves of 2624 with 2024-T351 and 2324-T39 and fatigue crack growth resistance of 2624 with 2024-T351 and 2324-T39.
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Published: 01 January 2000
Fig. 2 Typical stress relaxation curves plotted for (a) remaining stress and (b) relaxed stress (the initial stress minus the remaining stress). Source: Ref 11
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in Effect of Heat Treatment on Mechanical Properties of Titanium Alloys[1]
> Heat Treating of Nonferrous Alloys
Published: 01 June 2016
Fig. 23 Curves depicting stress versus cycles to failure ( R = –1) for Ti-1100 near-alpha titanium alloy. (a) Full lamellar microstructures showing range of effects of prior-beta grain sizes. (b) Duplex microstructures showing range of effects of primary alpha content
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Published: 01 January 2000
Fig. 7 Influence of stress triaxiality on J R -curves above initiation J I . Material: 22NiMoCr-3-7 mod; test temperature 80 °C (175 °F); ratio of crack length ( a ) to specimen width ( W ), 0.5
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Published: 01 January 2000
Fig. 5 Tensile stress-strain curves for copper, steel, and several thermoplastic resins. Source: Ref 8
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Published: 15 January 2021
Fig. 4 Creep curves produced under constant-load and constant-stress conditions. Reprinted with permission from Wiley. Source: Ref 6
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Published: 31 August 2017
Fig. 8 Tensile stress-strain curves indicating portions of total strain (TS) and recoverable strain (RS) of gray iron with type A graphite. UTS, ultimate tensile strength. Source: Ref 16
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in Effects of Process-Induced Defects on Fatigue Properties of Laser Powder Bed Fusion Metallic Materials
> Additive Manufacturing Design and Applications
Published: 30 June 2023
Fig. 7 Stress/cycles-to-failure curves for L-PBF-processed AlSi10Mg tested at R = 0.1. The L-PBF data are compared with the fatigue properties of cast AlSi10Mg. Fatigue data obtained from Ref 33 – 38
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in Effects of Process-Induced Defects on Fatigue Properties of Laser Powder Bed Fusion Metallic Materials
> Additive Manufacturing Design and Applications
Published: 30 June 2023
Fig. 8 Stress/cycles-to-failure curves for L-PBF-processed Ti-6Al-4V tested at R = 0.1. The L-PBF data are compared with the reference data from Metallic Materials Properties Development and Standardization (MMPDS). HIP, hot isostatic pressing. Fatigue data obtained from Ref 43 – 51
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Published: 15 June 2019
Fig. 3 Stress-life ( S - N ) fatigue curves (open hole, K t,net = 2.3, R = 0.1) for 7085-T7452 and 7050-T7452 die forgings
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in Mechanical Testing and Properties of Plastics—An Introduction
> Characterization and Failure Analysis of Plastics
Published: 15 May 2022
Fig. 2 Tensile stress-strain curves for copper, steel, and several thermoplastic resins. Source: Ref 5
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in Alclad 2029: High-Strength, High-Toughness Sheet/Plate
> Properties and Selection of Aluminum Alloys
Published: 15 June 2019
Fig. 1 Plane stress fracture toughness of alloys 2029 and 2024. (a) Strength toughness minima of fuselage alloys. (b) Plane stress R -curve
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Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006601
EISBN: 978-1-62708-210-5
...) 104 (95) T-L 13–15 (0.5–0.6) 104 (95) T-L Note: Minimum values 400 mm (16 in.) wide panel Fig. 1 Plane stress fracture toughness of alloys 2029 and 2024. (a) Strength toughness minima of fuselage alloys. (b) Plane stress R -curve Fig. 2 Fatigue crack growth (FCG...
Abstract
This datasheet provides information on key alloy metallurgy and applications of Alclad 2029. It contains tables that present statistically determined mechanical property minimums for Alclad 2029-T8 sheet and plate. The plane stress fracture toughness and fatigue crack growth resistance of alloys 2029 and 2024 are illustrated.
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003513
EISBN: 978-1-62708-180-1
... is, essentially, a graphical model, shown schematically in Fig. 2 , that reflects the stress-strain curve of the material. The FAD consists of two elements: the failure assessment curve (FAC) and the failure assessment point (FAP). The collapse ratio, S r or L r , is the ratio of the applied stress...
Abstract
Optimized modeling of fracture-critical structural components and connections requires the application of elastic-plastic fracture mechanics. Such applications, however, can require sophisticated analytical techniques such as crack tip opening displacement (CTOD), failure assessment diagram (FAD), and deformation plasticity failure assessment diagram (DPFAD). This article presents the origin and description of FAD and addresses R6 FAD using J-integral. It details the fracture criteria of BS 7910. The factors to be considered during the use of FAD and the applications of FAD are also reviewed.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003382
EISBN: 978-1-62708-195-5
... - N curve represents one loading type, as defined by its stress ratio, R =σ min /σ max , where σ min and σ max are the minimum and maximum stress, respectively. In the safe life approach, the S - N relation is used in design to establish a maximum allowable stress (or strain) and/or to predict...
Abstract
In the design of composite structures for durability and damage tolerance, the primary concerns are out-of-plane failures, such as delamination, material degradation associated with environment, stability under compression loading, large degree of scatter in fatigue life, and bearing failure of joints. This article presents an introductory discussion on the fatigue damage process, methodologies assessing fatigue behavior, and life prediction models. It describes the damage mechanisms introduced for a quasi-isotropic laminate under tension-compression fatigue loading. Delamination is a critical issue in fatigue and generally results from high interlaminar normal and shear stresses. The article schematically illustrates the structural elements in which high interlaminar stresses are common. It concludes with a discussion on the classification of fatigue models such as mechanistic or phenomenological, for composite materials under cyclic loading.
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003312
EISBN: 978-1-62708-176-4
... the CNB method and Y min * is the minimum stress intensity factor coefficient for the relevant geometry ( Ref 17 , 18 ). Interferences addressed in ASTM C 1421 include slow crack growth (i.e., environmentally assisted crack growth), R -curve effects, and stability. Other methods...
Abstract
Catastrophic failure best typifies the characteristic behavior of brittle solids in the presence of cracks or crack-like flaws under ambient conditions. This article provides a description of the concepts of fracture mechanics of brittle solids and focuses on the various testing methods developed to characterize the fracture behavior of brittle solids with examples. These include the fracture toughness test method and R-curve test method at ambient and elevated temperatures. The article also includes information on the evaluation of fracture-toughness test results and the behavior of R-curve.
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003261
EISBN: 978-1-62708-176-4
... steels. Due to its higher yield strength, the high-carbon spring steel has the greater resilience. Fig. 5 Comparison of stress-strain curves for high- and low-toughness steels. Cross-hatched regions in this curve represent the modulus of resilience ( U R ) of the two materials. The U R...
Abstract
This article focuses on mechanical behavior of materials under conditions of uniaxial tension and compression. The emphasis is on mechanical behavior during the engineering tension test, which is used to provide basic design information on the strength of materials and as an acceptance test for the specification of materials. The article presents mathematical expressions for a flow curve of many metals in the region of uniform plastic deformation. It explains that the rate at which strain is applied to the tension specimen has an important influence on the stress-strain curve. The point of necking at maximum load can be obtained from the true stress-true strain curve by finding the point on the curve having a subtangent of unity. The article concludes with an overview of the ductility measurements performed by notch tensile and compression tests.
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Published: 01 January 2000
Fig. 5 Comparison of stress-strain curves for high- and low-toughness steels. Cross-hatched regions in this curve represent the modulus of resilience ( U R ) of the two materials. The U R is determined by measuring the area under the stress-strain curve up to the elastic limit
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Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003311
EISBN: 978-1-62708-176-4
... the symbol R , and the resistance to crack growth, expressed in terms of the stress intensity factor, is given the symbol K R . The plot of resistance to crack growth, either R or K R , versus crack length is called a crack growth resistance curve, or R -curve, and the entire curve becomes...
Abstract
This article introduces the concepts of linear-elastic fracture mechanics (LEFM) and elastic-plastic fracture mechanics (EPFM). It reviews the fracture mechanics of ceramics and ceramic matrix composites (CMCs). The article describes some fracture toughness measurement techniques used on ceramics and CMCs: single edge notch bending, compact tension, double cantilever beam testing, chevron notch methods, and double torsion. It presents descriptions organized by their specimen types, and includes the advantages and disadvantages, as well as the experimental control schemes employed for each specimen type.
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