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Published: 15 June 2019
Fig. 1 Plane stress R -curves of 2624 compared with 2024-T351 and 2324-T39 More
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...
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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 More
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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 More
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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 More
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Published: 01 January 2000
Fig. 5 Tensile stress-strain curves for copper, steel, and several thermoplastic resins. Source: Ref 8 More
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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 More
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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 More
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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 More
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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 More
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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 More
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Published: 15 May 2022
Fig. 2 Tensile stress-strain curves for copper, steel, and several thermoplastic resins. Source: Ref 5 More
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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 More
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...
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...
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...
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...
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...
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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 More
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...