1-20 of 1375

Search Results for fatigue failures

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Book Chapter

Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003544
EISBN: 978-1-62708-180-1
... so. Many service failures still occur by fatigue, despite the well-defined characterization of fatigue properties in the laboratory. In part, the difficulty is that fatigue behavior is influenced by a great many variables such as the magnitude and frequency of application of the fluctuating...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006779
EISBN: 978-1-62708-295-2
... Abstract Fatigue failures may occur in components subjected to fluctuating (time-dependent) loading as a result of progressive localized permanent damage described by the stages of crack initiation, cyclic crack propagation, and subsequent final fracture after a given number of load...
Image
Published: 01 January 2002
Fig. 16 Fatigue failures. (a) Fatigue (upper right) changing to ductile failure (lower left). (b) Fatigue fracture of class 30 gray iron. (c) Single overload fracture of class 30 gray iron More
Image
Published: 15 January 2021
Fig. 16 Fatigue failures. (a) Fatigue (upper right) changing to ductile failure (lower left). (b) Fatigue fracture of class 30 gray iron. (c) Single overload fracture of class 30 gray iron More
Image
Published: 15 January 2021
Fig. 16 Fatigue failures with different fatigue crack size/final fracture ratios. (a) High stress level, low toughness. (b) Low stress level, high toughness More
Image
Published: 01 January 2006
Fig. 15 Micrographs characteristic of stage III fatigue failures. (a) Ti-6Al-7Nb alloy that failed by cleavage-type fracture. (b) Ti-6Al-4V ELI alloy that failed by ductile overload fracture More
Image
Published: 01 June 2012
Fig. 15 Micrographs characteristic of stage III fatigue failures. (a) Ti-6Al-7Nb alloy that failed by cleavage-type fracture. (b) Ti-6Al-4V ELI alloy that failed by ductile overload fracture More
Series: ASM Handbook
Volume: 11B
Publisher: ASM International
Published: 15 May 2022
DOI: 10.31399/asm.hb.v11B.a0006940
EISBN: 978-1-62708-395-9
... Abstract Failure of structural polymeric materials under cyclic application of stress or strain is a subject of industrial importance. The understanding of fatigue mechanisms (damage) and the development of constitutive equations for damage evolution, leading to crack initiation and propagation...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002353
EISBN: 978-1-62708-193-1
... Abstract Fatigue damage in metals is caused by the simultaneous action of cyclic stress, tensile stress, and plastic strain. This article details the fundamental aspects of the stages of the fatigue failure process. These include cyclic plastic deformation prior to fatigue crack initiation...
Image
Published: 01 January 2002
Fig. 24 Rotating bending fatigue failure of keyed medium-carbon steel shaft. Fatigue initiated at a corner of the keyway, as marked. Beach marks in that vicinity are concentric about the origin. As the fatigue crack grew, the bending stress distribution produced more rapid growth near More
Image
Published: 15 May 2022
Fig. 3 Thermal fatigue failure and conventional fatigue crack-propagation fracture during reversed-load cycling of acetal. Source: Ref 36 More
Image
Published: 15 January 2021
Fig. 24 Rotating-bending fatigue failure of keyed medium-carbon steel shaft. Fatigue initiated at a corner of the keyway, as marked. Beach marks in that vicinity are concentric about the origin. As the fatigue crack grew, the bending-stress distribution produced more rapid growth near More
Image
Published: 01 January 1987
Fig. 50 Fatigue failure of a bolt due to unidirectional cycling bending loads. The failure started at the thread root (arrow) and progressed across most of the cross section before final fast fracture. Actual size. More
Image
Published: 01 January 1987
Fig. 110 Macrograph (a) of defect in test bar that initiated fatigue failure. 1.5×. (b) SEM fractograph showing that the defect was a shrinkage cavity. Note the dendritic appearance. 375× More
Image
Published: 01 January 1987
Fig. 219 Fractograph of fatigue failure in SAE 1050 pin, induction hardened to a depth of 5 mm ( 3 16 in.) and surface hardness of 55 HRC. Core hardness: 21 HRC. Fatigue initiated inside the grease hole at the metallurgical notch created by the very sharp case-core hardness gradient More
Image
Published: 01 January 1987
Fig. 1335 Fatigue failure of an ultrasonically bonded aluminum transistor base lead, 25 μm (1 mil) in diameter. The transistor was power cycled until bond failure occurred. SEM, 1500× (R.J. Schwinghamer, NASA Marshall Space Flight Center) More
Image
Published: 01 January 1987
Fig. 291 Fatigue failure of flat, cantilever-type AISI 1070 spring due to inadequate removal of blanking fracture. Failure initiated at a point on the edge of the spring. SEM, 100× (J.H. Maker, Associated Spring, Barnes Group Inc.) More
Image
Published: 01 January 1987
Fig. 305 Fatigue failure of an automotive engine valve spring made of a steel similar to ASTM A230. The spring was shot peened; service stresses were very high. Cause of fracture was a seam 15 μm (0.5 mils) deep. The surface defect initiated a longitudinal shear crack that propagated More
Image
Published: 01 January 2002
Fig. 26 Fatigue failure of fasteners in single-lop shear carbon-graphite composite joints. (a) Fastener pullout resulting from a static tensile load. (b) Fatigue failure of fasteners initiated by cocking of the fasteners. Both 1 1 3 × More
Image
Published: 01 January 2002
Fig. 14 Fatigue failure of a low-alloy steel part. Shear lips around most of the periphery (as at arrows) as well as chevron marks over most of the fracture surface aid in identifying the fatigue fracture area at the lower left corner. Source: Ref 15 More