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Published: 01 January 1993
Fig. 14 Isothermal fatigue life calculation for thermal fatigue resistance approximation. (a) Package/solder joint geometry. L is the package size (distance between solder joints), α i is the thermal expansion coefficient, and t is the solder joint gap. (b) Fatigue life versus total shear More
Image
Published: 01 January 1993
Fig. 2 Isothermal fatigue life (plastic strain dependence) of bulk 60Sn-40Pb solder. Source: Ref 10 More
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002413
EISBN: 978-1-62708-193-1
... Abstract This article focuses on the isothermal fatigue of solder materials. It discusses the effect of strain range, frequency, hold time, temperature, and environment on isothermal fatigue life. The article provides information on various isothermal fatigue testing methods used to assess...
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Published: 01 January 2000
Fig. 29 Creep-fatigue interaction effects on isothermal cyclic life of AISI type 304 stainless steel tested in air at 650 °C (1200 °F), normal straining rate of 4 × 10 −3 s −1 . After Ref 65 More
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003314
EISBN: 978-1-62708-176-4
... load cells extensometry strain measuring devices environmental chambers graphic recorders furnaces heating systems baseline isothermal fatigue testing creep-fatigue interaction thermomechanical fatigue fatigue resistance Fatigue closed loop control advanced software tools fatigue life...
Series: ASM Handbook
Volume: 7
Publisher: ASM International
Published: 30 September 2015
DOI: 10.31399/asm.hb.v07.a0006094
EISBN: 978-1-62708-175-7
... engines, experience many throttle changes during flight, requiring extended low-cycle fatigue life as engine loads rise and fall. By comparison, auxiliary power units run more like diesel engines, rising to full load after start up, and running steadily in this range for nearly entire flights. Although...
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Published: 01 January 1996
Fig. 13 Strain-fatigue curves for 2 1 4 Cr-1Mo steel (class 1) at 425 °C (800 °F) with comparison of strain life at 595 °C (1100 °F). Open points, annealed; solid points, isothermally annealed. R = −1. Source: Ref 18 More
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002391
EISBN: 978-1-62708-193-1
.... A distinction must be drawn between isothermal high-temperature fatigue as cyclic straining under constant nominal temperature conditions versus TMF. As such, isothermal fatigue (IF) can be considered a special case of TMF. In most the deformation and fatigue damage under TMF cannot be predicted based...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006781
EISBN: 978-1-62708-295-2
... damage mechanisms and elucidate mechanism coupling interactions. In addition, life modeling in TMF conditions and a practical application of TMF life prediction are presented. coupling interactions fatigue life prediction thermomechanical fatigue THERMOMECHANICAL FATIGUE (TMF) is the general...
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
... 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...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002469
EISBN: 978-1-62708-194-8
... is the discussion of design considerations against fatigue related to material performance under mechanical loading at constant temperature (isothermal fatigue, or simply fatigue). In this article, periodic loading of specimens is considered, and the material properties related to fatigue derived from these tests...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003545
EISBN: 978-1-62708-180-1
... and associated failures of alloys used in high-temperature applications. The complex effects of creep-fatigue interaction are also discussed, although more detail on this is described in the article “Thermomechanical Fatigue: Mechanisms and Practical Life Analysis” in this Volume. Life assessment is also...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006780
EISBN: 978-1-62708-295-2
... in high-temperature applications. The complex effects of creep-fatigue interaction are also discussed, although more detail on this is described in the article “Thermomechanical Fatigue: Mechanisms and Practical Life Analysis” in this Volume. Life assessment is also covered in the article “Elevated...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003517
EISBN: 978-1-62708-180-1
.... The article discusses metallurgical instabilities of steel-based alloys and nickel-base superalloys. It provides information on several life assessment methods, namely, the life fraction rule, parameter-based assessments, the thermal-mechanical fatigue, coating evaluations, hardness testing, microstructural...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003546
EISBN: 978-1-62708-180-1
... Abstract Thermomechanical fatigue (TMF) refers to the process of fatigue damage under simultaneous changes in temperature and mechanical strain. This article reviews the process of TMF with a practical example of life assessment. It describes TMF damages caused due to two possible types...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0005723
EISBN: 978-1-62708-193-1
... A(T) arc tension specimen field) A(T) arc-shaped specimen (in tension) a0 mean stress in strain life method I moment of inertia ATC accelerated thermal cycling =(0"3 stress amplitude, O"a O"max- O"min)/2 IF isothermal fatigue a/W crack length to depth ratio O"ce critical stress in emergency condition...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.9781627081931
EISBN: 978-1-62708-193-1
Series: ASM Handbook
Volume: 4A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v04a.a0005788
EISBN: 978-1-62708-165-8
... pulsating sinusoidal loads, with a frequency of 16 Hz and a stress ratio, R , of 0. Test results ( 10 ) are plotted as S - N curves, that is, plots of nominal stress amplitude versus fatigue life (number of cycles) to initial cracking. Even though the number of tests was low, it can still be concluded...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002402
EISBN: 978-1-62708-193-1
... for 2 1 4 Cr-1Mo steel (class 1) at 425 °C (800 °F) with comparison of strain life at 595 °C (1100 °F). Open points, annealed; solid points, isothermally annealed. R = −1. Source: Ref 18 Fig. 14 Strain-fatigue for 2 1 4 Cr-1 Mo steel (class 1) at three temperatures...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002376
EISBN: 978-1-62708-193-1
... Abstract This article provides information on the nominal compositions of high-carbon bearing steels and carburizing bearing steels. It discusses the bearing fundamentals with emphasis on surface contact, stresses, and fatigue life of bearings. The article describes bearing life prediction...