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smooth specimens
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Image
Published: 01 March 2006
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Published: 01 December 1999
Fig. 7.28 Fatigue graphs for smooth specimens from (a) steel ShKh 15 tempered at 200 °C and (b) steel 50KhN tempered at 150 °C. Source: Ref 45
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Image
Published: 01 July 2009
Fig. 17.45 Comparison of axial fatigue strength of smooth specimens of beryllium, titanium (Ti-6Al-4V), and aluminum (7075-T6). Source: Brush Wellman 2001
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Image
Published: 01 July 2000
Fig. 7.93 Effect of artificial aging at 320 °F on the strength and smooth-specimen SCC threshold stress of 7075-T651 and 7178-T651 aluminum alloys. Source: Ref 97
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.75 Fatigue curves for smooth rotating beam specimens of steel 45 tested in air and in 3% NaCl solution before and after nitriding. Source: Ref 11.81
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Image
Published: 01 December 2004
Fig. A3.2 Test sections of (a) smooth and (b) notched rotating beam fatigue specimens. Dimensions in inches
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in Petroleum Reactor Pressure-Vessel Materials for Hydrogen Service
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 7.30. Creep-test results at 550 °C (1020 °F) for smooth and notched specimens of synthetic HAZ material (peak temperature, 1350 °C, or 2460 °F) in 1¼Cr-½lMo and 2¼Cr-1Mo steel (theoretical stress-concentration factor for notched specimen, 1.9) ( Ref 6 ).
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Image
Published: 01 July 2009
Fig. 17.7 Elongation as a function of temperature for smooth bar specimens from vacuum hot-pressed blocks of S-65B (solid line) and S-200E (broken line) beryllium. Included are results of a competing graphite product. Source: Smith et al. 1985
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in Stress-Corrosion Cracking of High-Strength Steels (Yield Strengths Greater Than 1240 MPa)[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 3.19 Alternate-immersion stress-corrosion data from smooth bend specimens. Source: Ref 3.8
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Image
Published: 01 July 2009
Fig. 4.4 Young’s modulus as a function of temperature for smooth-bar specimens from vacuum hot pressed blocks of S-65B and S-200E beryllium. Included are results of a competing graphite product. Source: Smith et al. 1985
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140253
EISBN: 978-1-62708-335-5
... or average properties for the individual alloys and tempers. In some cases, the results of tests from several lots of the same alloy and temper are included on one figure. Unless otherwise noted, the tests are performed on smooth and notched specimens as shown in Fig. A3.2 of Appendix 3...
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140301
EISBN: 978-1-62708-335-5
... are of the same magnitude. The notched rotating beam fatigue specimens were similar to the smooth specimens, but contained a sharp V-notch in the center of the test section, providing a theoretical stress concentration factor ≥ 19. Rotating beam specimens with slight variations in design are presented. Figure...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090367
EISBN: 978-1-62708-266-2
... strain, plastic strain, and residual stress responses. It also describes the difference between smooth and precracked specimens and how they are used, provides information on slow-strain-rate testing and how to assess the results, and discusses various test environments and procedures, including tests...
Abstract
This chapter addresses the challenge of selecting an appropriate stress-corrosion cracking (SCC) test to evaluate the serviceability of a material for a given application. It begins by establishing a generic model in which SCC is depicted in two stages, initiation and propagation, that further subdivide into several zones plus a transition region. It then discusses SCC test standards before describing basic test objectives and selection criteria. The chapter explains how to achieve the required loading conditions for different tests and how to prepare test specimens to determine elastic strain, plastic strain, and residual stress responses. It also describes the difference between smooth and precracked specimens and how they are used, provides information on slow-strain-rate testing and how to assess the results, and discusses various test environments and procedures, including tests for weldments. The chapter concludes with a section on how to interpret time to failure, threshold stress, percent survival, stress intensity, and propagation rate data, and assess the precision of the associated tests.
Image
Published: 01 December 2000
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in Rotating-Beam Reversed-Bending Fatigue Curves
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. D6.101 518.0-F, die cast aluminum casting rotating-beam fatigue curve. Smooth and notched specimens from one lot. Smooth specimens per Fig. A3.4, Appendix 3 . Machined notched specimens per Fig. A3.2(b), Appendix 3 . As-cast notched specimen has radius <0.01 in.
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in Rotating-Beam Reversed-Bending Fatigue Curves
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. D6.94 390.0-F, die cast aluminum casting rotating-beam fatigue curve. Smooth and notched specimens from one lot. Smooth specimens per Fig. A3.7, Appendix 3 . Notched specimens similar to Fig. A3.2(b), Appendix 3 , except notch radius is as noted
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in Rotating-Beam Reversed-Bending Fatigue Curves
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. D6.100 518.0-F, die cast aluminum casting rotating-beam fatigue curve. Smooth and notched specimens from one lot, with comparison to prior test. Smooth specimens per Fig. A3.4, Appendix 3 . Notched specimens similar to Fig. A3.2(b), Appendix 3 , except notch radius is as noted
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in Rotating-Beam Reversed-Bending Fatigue Curves
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. D6.17 249.0-T63, sand cast aluminum casting rotating-beam fatigue curve. Circles are smooth and notched specimens from one lot. Squares are smooth specimens taken from cast slab
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Published: 01 December 2004
Fig. A3.3 Reduced smooth rotating beam fatigue specimen, same as used by U.S. Naval Engineering Experiment Station
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Published: 01 December 2004
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