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fatigue stress

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Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004208
EISBN: 978-1-62708-184-9
... Abstract This article provides information on biomedical aspects such as active biological responses and the chemical environment characterizing the internal physiological milieu, as well as electrochemical fundamentals needed for characterizing corrosion fatigue (CF) and stress-corrosion...
Series: ASM Handbook
Volume: 23
Publisher: ASM International
Published: 01 June 2012
DOI: 10.31399/asm.hb.v23.a0005654
EISBN: 978-1-62708-198-6
... Abstract This article describes mechanical/electrochemical phenomena related to in vivo degradation of metals used for biomedical applications. It discusses the properties and failure of these materials as they relate to stress-corrosion cracking (SCC) and corrosion fatigue (CF). The article...
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Published: 31 December 2017
Fig. 5 Cycles to failure versus maximum fatigue stress for carbon-implanted and unimplanted Ti-6Al-4V. Normal stress, 690 MPa (100 ksi); baseline fatigue (no fretting) data, 20.7 MPa (3 ksi). Source: Ref 10 , 27 More
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Published: 01 December 1998
Fig. 19 Types of fatigue test stress. (a) Alternating stress in which S m = 0 and R = −1. (b) Pulsating tensile stress in which S m = S a , the minimum stress is zero, and R = 0. (c) Fluctuating tensile strength in which both the minimum and maximum stresses are tensile stresses More
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Published: 30 November 2018
Fig. 6 Stress/number of cycles to fatigue curves resulting from stress-controlled fatigue testing of powder metallurgy aluminum alloy AC-2236, fully reversed (R = −1). Machined test bars, axial loading. Source: Ref 63 More
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Published: 30 November 2018
Fig. 7 Stress/number of cycles to fatigue curves resulting from stress-controlled fatigue testing of powder metallurgy aluminum alloy AC-2236, in tensile mode only (R = 0.1) More
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Published: 01 January 1990
Fig. 1 Types of fatigue test stress. (a) Alternating stress in which S m = 0 and R = −1. (b) Pulsating tensile stress in which S m = S a , the minimum stress is zero, and R = 0. (c) Fluctuating tensile stress in which both the minimum and maximum stresses are tensile stresses More
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Published: 30 September 2015
Fig. 13 Hertz contact stress. Typical contact stress distribution for fatigue loaded components. Courtesy of PMG More
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Published: 01 January 1996
Fig. 20 Fatigue limit diagram relating stress amplitude and mean stress of materials at different tensile strength levels. Source: Ref 7 More
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Published: 01 January 1996
Fig. 53 Effect of stress ratio on fatigue threshold stress-intensity factor range, Δ K th , for A533B-1 steel. Data are for A533B-1 steel in region 1, tested at various stress ratios, at 60 Hz and 25 °C (75 °F) in air. Source: Ref 17 More
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Published: 01 January 1996
Fig. 55 Effect of stress ratio on fatigue threshold stress-intensity factor range, Δ K th , for several steels. Source: Ref 17 More
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Published: 01 January 1996
Fig. 2 Universal fatigue plot of normalized stress (stress on specimen divided by fracture stress at −196 °C), σ/σ N versus log ( t / t 0.5 ) (load duration divided by the load duration at σ/σ N = 0.5). Data are for abraded soda-lime-silica specimens and are taken from Ref 6 . More
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003316
EISBN: 978-1-62708-176-4
... Abstract Fretting is a special wear process that occurs at the contact area between two materials under load and subject to slight relative movement by vibration or some other force. During fretting fatigue, cracks can initiate at very low stresses, well below the fatigue limit of nonfretted...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002415
EISBN: 978-1-62708-193-1
.... It discusses the fatigue behavior of composite laminates in the form of a relation between applied maximum fatigue stress and fatigue life. The article explains Weibull distribution and parameters estimation for fatigue data analysis and life prediction of composite laminates. It analyzes the fatigue...
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Published: 01 January 1987
Fig. 90 Fatigue fractures in Inconel X-750 tested at a stress intensity of Δ K = 20 MPa m (18 ksi in. ) in air and vacuum at 650 °C (1200 °F). The crack propagation direction is from bottom to top. The fracture in air (a) exhibited a faceted, crystallographic appearance More
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Published: 01 January 1987
Fig. 1247 Surface of a high-cycle fatigue fracture in a stress-relieved specimen of 90Ta-10W alloy sheet containing a central transverse notch 5 mm (0.2 in.) wide. Tensile strength was 552 MPa (80 ksi). The specimen was loaded in tension at room temperature to a stress cycled from 80 to 400 More
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Published: 01 January 2002
Fig. 15 Stress fields and corresponding torsional-fatigue cracks. (a) and (b) Shaft with keyway. (c) Shaft with splines More
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Published: 01 January 2002
Fig. 37 Stainless steel superheater tube that failed by thermal fatigue and stress rupture. (a) Photograph of the tube showing thick-lip rupture. (b) Macrograph of a section taken transverse to a fracture surface of the tube showing that thermal fatigue cracking started at the outside surface More
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Published: 01 January 2002
Fig. 34 Fatigue-crack-initiation behavior of various steels at a stress ratio of +0.1. Source: Ref 9 More
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Published: 01 January 2002
Fig. 2 Stress risers initiating rolling-contact fatigue failure More