Skip Nav Destination
Close Modal
Search Results for
fatigue stress
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 1989 Search Results for
fatigue stress
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
1
Sort by
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...
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 cracking (SCC). It discusses some of the mechanical and electrochemical phenomena related to the in vivo degradation of materials used for biomedical applications. These materials include stainless steels, cobalt and titanium-base alloy systems, and dental amalgam. The article addresses key issues related to the simulation of the in vivo environment, service conditions, and data interpretation. The factors influencing susceptibility to CF and SCC are reviewed. The article describes the testing methodology of CF and SCC. It also summarizes findings from laboratory testing, in vivo testing and retrieval studies related to CF and SCC.
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...
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 presents the factors related to the use of surgical implants and their deterioration in the body environment, including biomedical aspects, chemical environment, and electrochemical fundamentals needed for characterizing CF and SCC. It provides a discussion on the use of metallic biomaterials in surgical implant applications, such as orthopedic, cardiovascular surgery, and dentistry. It addresses key issues related to the simulation of an in vivo environment, service conditions, and data interpretation. These include the frequency of dynamic loading, electrolyte chemistry, applicable loading modes, cracking mode superposition, and surface area effects. The article explains the fundamentals of CF and SCC, and presents the test findings from laboratory, in vivo, and retrieval studies.
Image
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
Image
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
Image
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
Image
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
Image
in Fatigue Resistance of Steels
> Properties and Selection: Irons, Steels, and High-Performance Alloys
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
Image
Published: 30 September 2015
Fig. 13 Hertz contact stress. Typical contact stress distribution for fatigue loaded components. Courtesy of PMG
More
Image
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
Image
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
Image
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
Image
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...
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 specimens. This article describes the mechanisms of fretting and fretting fatigue; stress analysis, modeling, and prediction of fretting fatigue; fretting fatigue testing; and fretting prevention methods. Three general geometries and loading conditions for fretting fatigue, along with their remedies, are reviewed.
Book Chapter
Book: Fatigue and Fracture
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...
Abstract
Knowledge of fatigue behavior at the laminate level is essential for understanding the fatigue life of a laminated composite structure. This article describes fatigue failure of composite laminates in terms of layer cracking, delamination, and fiber break and interface debonding. 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 properties and damage tolerance of fiber-metal laminates such as ARALL and GLARE laminates. The article concludes with a discussion on the effects of fatigue on notched and unnotched specimens.
Image
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
Image
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
Image
Published: 01 January 2002
Fig. 15 Stress fields and corresponding torsional-fatigue cracks. (a) and (b) Shaft with keyway. (c) Shaft with splines
More
Image
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
Image
Published: 01 January 2002
Fig. 34 Fatigue-crack-initiation behavior of various steels at a stress ratio of +0.1. Source: Ref 9
More
Image
Published: 01 January 2002
1