Skip Nav Destination
Close Modal
Search Results for
fatigue crack growth
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 569
Search Results for fatigue crack growth
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
1
Sort by
Image
Influence of texture on fatigue crack growth in Ti-6Al-4V. Fatigue crack gr...
Available to Purchase
in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 58 Influence of texture on fatigue crack growth in Ti-6Al-4V. Fatigue crack growth rates are higher when basal planes are loaded in tension. The elastic modulus in tension for the basal texture (B) is 109 GPa (15.8 × 10 6 psi); for the transverse texture (T), 126 GPa (18.3 × 10 6 psi
More
Image
Fatigue crack growth testing and data analysis. (a) Crack length measuremen...
Available to PurchasePublished: 30 June 2023
Fig. 9.16 Fatigue crack growth testing and data analysis. (a) Crack length measurement, (b) calculation of crack growth rate, and (c) analysis of da/dN versus stress intensity range.
More
Image
Fatigue crack growth behavior of 7075-T6 aluminum under remote and crack-li...
Available to PurchasePublished: 01 August 2005
Fig. 5.40 Fatigue crack growth behavior of 7075-T6 aluminum under remote and crack-line loading conditions. Source: Ref 5.41
More
Image
Fatigue crack growth per fatigue cycle ( da / dN ) versus stress intensity ...
Available to PurchasePublished: 01 October 2011
Fig. 7.25 Fatigue crack growth per fatigue cycle ( da / dN ) versus stress intensity variation ( Δ K ) per cycle. The C and n are constants that can be obtained from the intercept and slope, respectively, of the linear log da / dN versus log Δ K plot. This equation for fatigue crack
More
Image
A typical fatigue-crack growth-rate curve consists of three regions: a slow...
Available to PurchasePublished: 30 November 2013
Fig. 14 A typical fatigue-crack growth-rate curve consists of three regions: a slow-growing region (threshold), a linear region (the middle section of the curve), and a terminal region toward the end of the curve where Δ K approaches K c . The Paris power-law equation, da/dN = C (Δ K
More
Image
Published: 01 June 2008
Image
Fatigue crack growth rate results for two A588 grade A HSLA steels showing ...
Available to PurchasePublished: 01 December 2001
Fig. 21 Fatigue crack growth rate results for two A588 grade A HSLA steels showing comparison of LS and SL testing orientations. CON, conventional; CaT, calcium treatment. Improved isotropy of the calcium-treated steel is noted.
More
Image
Published: 01 December 2001
Fig. 22 Range of fatigue crack growth notes at Δ k = 55 MPa m (50 ksi in ) in six testing orientations for conventional (CON) and calcium-treated (CaT) quality plates of A516-70, A533B-1, and A514F. Improved isotropy of quality levels is demonstrated for calcium-treated
More
Image
in Properties and Performance of Aluminum Castings
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. 8.26 Fatigue crack growth rate ( R = 0.1) versus stress-intensity factor at room temperature for A356.0-T6 aluminum alloy castings produced by various processes
More
Image
in Properties and Performance of Aluminum Castings
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. 8.27 Fatigue crack growth rate ( R = 0.5) versus stress-intensity factor at room temperature for A356.0-T6 aluminum alloy castings produced by various processes
More
Image
Effect of hold time on fatigue-crack-growth-rate properties of 2¼Cr-1Mo cas...
Available to Purchase
in Life Assessment of Steam-Turbine Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 6.40. Effect of hold time on fatigue-crack-growth-rate properties of 2¼Cr-1Mo cast steel ( Ref 91 ).
More
Image
Fatigue-crack-growth-rate data for ESR 12Cr-Mo-V rotor steel at 20, 550, an...
Available to Purchase
in Materials for Advanced Steam Plants
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 8.22. Fatigue-crack-growth-rate data for ESR 12Cr-Mo-V rotor steel at 20, 550, and 600 °C compared with standard X21CrMoV121 alloy at 20 °C ( Ref 67 ).
More
Image
Fatigue-crack-growth rates as a function of cyclic stress-intensity range f...
Available to Purchase
in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.55. Fatigue-crack-growth rates as a function of cyclic stress-intensity range for IN 738 LC and IN 939 at 850 °C (1560 °F) in different environments ( Ref 9 and 84 ).
More
Image
Published: 01 December 1989
Image
Published: 01 December 1989
Image
Published: 01 December 1989
Image
Effect of temperature on fatigue-crack-growth behavior of 2¼Cr-1Mo steel ( ...
Available to PurchasePublished: 01 December 1989
Image
Fatigue-crack-growth rates of long cracks for various high-temperature allo...
Available to PurchasePublished: 01 December 1989
Fig. 4.47. Fatigue-crack-growth rates of long cracks for various high-temperature alloys in air at (left) room temperature and (right) 850 °C (1560 °F) ( Ref 186 ).
More
Image
Fatigue-crack-growth rates for Inconel X-750 as a function of stress-intens...
Available to PurchasePublished: 01 December 1989
Fig. 4.48. Fatigue-crack-growth rates for Inconel X-750 as a function of stress-intensity-factor range at a cycling frequency of 0.17 Hz ( Ref 185 ).
More
Image
Variation of fatigue-crack-growth rates as a function of temperature at ΔK ...
Available to PurchasePublished: 01 December 1989
Fig. 4.49. Variation of fatigue-crack-growth rates as a function of temperature at ΔK = 30 MPa m (27 ksi in . ).
More
1