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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...
Abstract
This article describes the phenomena of crack initiation and early growth. It examines specimen design and preparation as well as the apparatus used in crack initiation testing. The article provides descriptions of the various commercially available fatigue testing machines: axial fatigue testing machines and bending fatigue machines. Load cells, grips and alignment devices, extensometry and strain measuring devices, environmental chambers, graphic recorders, furnaces, and heating systems of ancillary equipment are discussed. The article presents technologies available to accomplish closed loop control of materials testing systems in performing standard materials tests and for the development of custom testing applications. It explores the advanced software tools for materials testing. The article includes a description of baseline isothermal fatigue testing, creep-fatigue interaction, and thermomechanical fatigue. The effects of various variables on fatigue resistance and guidelines for fatigue testing are also presented.
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Published: 01 December 1998
Fig. 37 Typical fatigue life test specimens. (a) Torsional specimen. (b) Rotating cantilever beam specimen. (c) Rotating beam specimen. (d) Plate specimen for cantilever reverse bending. (e) Axial loading specimen. The design and type of specimen used depend on the fatigue testing machine used
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Published: 01 January 1996
Fig. 9 Typical fatigue life test specimens. (a) Torsional specimen. (b) Rotating cantilever beam specimen. (c) Rotating beam specimen. (d) Plate specimen for cantilever reverse bending. (e) Axial loading specimen. The design and type of specimen used depend on the fatigue testing machine used
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Published: 01 June 2012
Fig. 21 Constant-life diagram from the diamond stent subcomponent fatigue testing where the various conditions of mean strain and strain amplitude are plotted. Conditions that survived the 10 7 cycle testing are shown as open symbols, whereas cyclic conditions that led to fracture at <10 7
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Book Chapter
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002420
EISBN: 978-1-62708-193-1
.... The effects of mean stress or strain on transition fatigue life are reviewed. The article describes the determination of four fatigue-life parameters either by curve fitting actual fatigue life test data or approximating the constants from tensile properties. It contains a table that lists the tensile...
Abstract
The four-point method to estimate fatigue life behavior from tensile properties allows the construction of fatigue life curves from more readily available handbook data. This article provides information on the strain-based four-point method and the stress-based four-point method. The effects of mean stress or strain on transition fatigue life are reviewed. The article describes the determination of four fatigue-life parameters either by curve fitting actual fatigue life test data or approximating the constants from tensile properties. It contains a table that lists the tensile properties of various alloys.
Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003241
EISBN: 978-1-62708-199-3
... Abstract This article reviews the various types of mechanical testing methods, including hardness testing; tension testing; compression testing; dynamic fracture testing; fracture toughness testing; fatigue life testing; fatigue crack growth testing; and creep, stress-rupture, and stress...
Abstract
This article reviews the various types of mechanical testing methods, including hardness testing; tension testing; compression testing; dynamic fracture testing; fracture toughness testing; fatigue life testing; fatigue crack growth testing; and creep, stress-rupture, and stress-relaxation testing. Shear testing, torsion testing, and formability testing are also discussed. The discussion of tension testing includes information about stress-strain curves and the properties described by them.
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Published: 30 November 2018
Fig. 9 Strain-controlled fatigue tests. Strain-life fatigue curves for metal-matrix composite with alumina contents from 0 to 15%. AS, as-sintered; HT, heat treated, T6. Source: Ref 71
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in Fatigue Resistance of Steels
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 21 Effect of case depth on fatigue life. Fatigue tests on induction-hardened 1038 steel automobile axle shafts 32 mm (1 1 4 in.) in diameter. Case depth ranges given on the chart are depths to 40 HRC. Shafts with lower fatigue life had a total case depth to 20 HRC of 4.5 to 5.2
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in Fatigue Resistance of Steels
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 8 Surface roughness correction factors for standard rotating-beam fatigue life testing of steel parts. See Table 1 for correction factors from part diameter and type of loading. Source: Ref 6
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Published: 01 December 1998
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Published: 01 December 1998
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Published: 01 January 2000
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Published: 15 May 2022
Fig. 10 Schematic of specimens used for total-life fatigue analysis. Tests can be done (a) in torsion, (b) with a rotating cantilever, (c) with a rotating beam, (d) with cantilever reverse bending, or (e) under axial loading.
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Published: 01 January 1990
Fig. 8 Fatigue-life distribution of 0.50 mm (0.020 in.) diam music wire. Tested in a rotating-beam machine at a maximum stress of 1170 MPa (170 ksi) and a mean stress of zero
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Published: 01 January 1996
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Published: 01 January 1996
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Published: 01 January 1996
Fig. 7 Effect of dwell time on fatigue life of powder metallurgy Inconel 100 tested at 650 °C (1200 °F). Tests with no dwell were conducted at 0.33 Hz. Source: Ref 69
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Published: 01 January 1996
Fig. 14 Effect of ramp time on fatigue life of 62Sn-36Pb-2Ag solder in tests with and without tensile hold time ( t ht ) (at 25 °C; no compressive hold time). Source: Ref 34
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Published: 01 January 1996
Fig. 15 Effect of tensile hold time on fatigue life of 62Sn-36Pb-2Ag solder in tests with different ramp times ( t t ) at 25 °C; no compressive hold time). Total strain range is 1%. Source: Ref 34
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Published: 01 January 2000
Fig. 1 Schematic of specimens used for total life fatigue analysis. Tests can be done (a) in torsion, (b) with a rotating cantilever, (c) with a rotating beam, (d) with cantilever reverse bending, or (e) under axial loading
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