Skip Nav Destination
Close Modal
Search Results for
stress failure
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 852 Search Results for
stress failure
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
Sort by
Image
Published: 01 July 2000
Fig. 7.91 Sustained tensile-stress failure time for 76 mm (3 in.) plate of 7075-T651 aluminum alloy. Shaded bands indicate combinations of stress and time known to produce SCC in specimens intermittently immersed in 3.5% NaCl solution. Point A is the minimum yield strength in the long transverse
More
Image
Published: 01 November 2010
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090419
EISBN: 978-1-62708-266-2
...Abstract Abstract This chapter describes nondestructive evaluation (NDE) test methods and their relative effectiveness for diagnosing the cause of stress-corrosion cracking (SCC) service failures. It discusses procedures for analyzing various types of damage in carbon and low-alloy steels, high...
Abstract
This chapter describes nondestructive evaluation (NDE) test methods and their relative effectiveness for diagnosing the cause of stress-corrosion cracking (SCC) service failures. It discusses procedures for analyzing various types of damage in carbon and low-alloy steels, high-strength low-alloy steels, hardenable stainless steels, austenitic stainless steels, copper-base alloys, titanium and titanium alloys, aluminum and aluminum alloys, and nickel and nickel alloys. It identifies material-environment combinations where SCC is known to occur, provides guidelines on how to characterize cracking and fracture damage, and explains what to look for during macroscopic and microscopic examinations as well as chemical and metallographic analyses. It also includes nearly a dozen case studies investigating SCC failures in various materials.
Image
Published: 01 March 2006
Fig. A.59 Probability of failure as a function of stress amplitude for a failure to occur before a specified number of cycles
More
Image
Published: 01 November 2012
Fig. 17 (a) Stress versus log cycles to failure curve. (b) Log stress versus log cycles to failure curve. Source: Ref 11
More
Image
in Stress-Corrosion Cracking of Zirconium Alloys[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 11.6 Effect of temperature on time to failure of stress split rings (stress = 310 MPa, or 45 ksi) of Zircaloy-2 with an iodine content, I 2 , of 3 × 10 −3 g/cm 2 . Source: Ref 11.18
More
Image
Published: 01 November 2012
Fig. 18 Stress versus log cycles to failure curves for bending and axial loading tests of 4340 steel. Source: Ref 11
More
Image
Published: 01 November 2012
Fig. 19 Log true stress versus log reversals to failure of 4340 steel. From Fatigue Design Handbook , SAE. Source: Ref 11
More
Image
Published: 01 November 2012
Fig. 18 Intergranular failure in nickel-base alloy. Inconel 751, stress rupture at 1350 °F, 55 ksi, 125 h. Source: Ref 8
More
Image
Published: 01 October 2012
Fig. 10.14 Stress amplitude-failure cycles ( S - N ) plot of 3 mol%-yttria-stabilized zirconia tensile specimens for various R -ratios. Solid lines show CARES/LIFE predictions at 50% reliability using the Walker slow crack growth law to predict strength degradation due to cyclic fatigue. Source
More
Image
Published: 01 February 2005
Image
Published: 01 January 2000
Fig. 53 Stress-corrosion failure of an Apollo Ti-6Al-4V RCS pressure vessel due to nitrogen tetroxide. (a) Failed vessel after exposure to pressurized N 2 O 4 for 34 h. (b) Cross section through typical stress-corrosion cracks. 250×
More
Image
Published: 01 January 2000
Fig. 54 Stress-corrosion failure of a type 304 stainless steel heat exchanger tube from carbon dioxide compressor intercooler after exposure to a pressurized chloride-containing (200 ppm) environment at 120 °C (250 °F) (a) Cracks on the external surface. (b) Cracks originating on the external
More
Image
Published: 01 December 2000
Fig. 12.16 Curves depicting stress versus cycles to failure for pure titanium as affected by (a) grain size, (b) oxygen content, and (c) cold work
More
Image
Published: 01 December 2000
Fig. 12.17 Curves depicting room-temperature stress versus cycles to failure for grade 2 titanium (0.03 wt% iron) at two temperatures. UTS, ultimate tensile strength
More
Image
Published: 01 December 2000
Fig. 12.18 Curves depicting room-temperature stress versus cycles to failure for alpha-beta titanium alloy Ti-6Al-4V in a variety of conditions. (a) Fully lamellar structure. (b) Fully equiaxed structure. (c) Duplex microstructure. In (a), width of alpha lamellae is at issue; in (b), effect
More
Image
Published: 01 December 2000
Fig. 12.20 Curves depicting stress versus cycles to failure (R = –1) for Ti-1100 near-alpha titanium alloy. (a) Full lamellar microstructures showing range of effects of prior-beta grain sizes. (b) Duplex microstructures showing range of effects of primary alpha content
More
Image
Published: 01 December 2000
Fig. 12.25 Curves depicting stress versus cycles to failure for various microstructures in Ti-10V-2Fe-3Al beta alloy for various levels of primary alpha. R = –1.
More
Image
Published: 01 December 2000
Fig. 12.27 Curves depicting stress versus cycles to failure for coarse-grained Ti-8Al alpha alloy with and without thermomechanical processing to produce local grain refinement at the surface
More
Image
Published: 01 December 2000
Fig. 12.28 Curves depicting stress versus cycles to failure for Ti-6Al-2Sn-4Zr-2Mo alloy with and without thermomechanical processing to produce local grain refinement at the surface
More