Skip Nav Destination
Close Modal
Search Results for
stress rupture
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 918 Search Results for
stress rupture
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
Book Chapter
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003545
EISBN: 978-1-62708-180-1
... Abstract This article reviews the applied aspects of creep and stress-rupture failures. It discusses the microstructural changes and bulk mechanical behavior of classical and nonclassical creep behavior. The article provides a description of microstructural changes and damage from creep...
Abstract
This article reviews the applied aspects of creep and stress-rupture failures. It discusses the microstructural changes and bulk mechanical behavior of classical and nonclassical creep behavior. The article provides a description of microstructural changes and damage from creep deformation, including stress-rupture fractures. It also describes metallurgical instabilities, such as aging and carbide reactions, and evaluates the complex effects of creep-fatigue interaction. The article concludes with a discussion on thermal fatigue and creep fatigue failures.
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006780
EISBN: 978-1-62708-295-2
... Abstract The principal types of elevated-temperature mechanical failure are creep and stress rupture, stress relaxation, low- and high-cycle fatigue, thermal fatigue, tension overload, and combinations of these, as modified by environment. This article briefly reviews the applied aspects...
Abstract
The principal types of elevated-temperature mechanical failure are creep and stress rupture, stress relaxation, low- and high-cycle fatigue, thermal fatigue, tension overload, and combinations of these, as modified by environment. This article briefly reviews the applied aspects of creep-related failures, where the mechanical strength of a material becomes limited by creep rather than by its elastic limit. The majority of information provided is applicable to metallic materials, and only general information regarding creep-related failures of polymeric materials is given. The article also reviews various factors related to creep behavior and associated failures of materials used in high-temperature applications. The complex effects of creep-fatigue interaction, microstructural changes during classical creep, and nondestructive creep damage assessment of metallic materials are also discussed. The article describes the fracture characteristics of stress rupture. Information on various metallurgical instabilities is also provided. The article presents a description of thermal-fatigue cracks, as distinguished from creep-rupture cracks.
Image
Published: 01 December 1998
Fig. 15 Effect of notch on stress-rupture behavior. Stress-rupture behavior of smooth ( K = 1.0) and notched specimens of Fe-0.27C-0.75Mn-0.65Si-1.25Cr-0.50Mo-0.85V steel tested at 595 °C (1100 °F). All specimens were normalized at 980 °C (1800 °F) and tempered at 6 h at 675 °C (1250 °F)
More
Image
in Elevated-Temperature Properties of Ferritic Steels
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 17 Effect of notch on stress-rupture behavior. Stress-rupture behavior of smooth ( K = 1.0) and notched specimens of AISI 603 steel tested at 595 °C (1100 °F). All specimens were normalized at 980 °C (1800 °F) and tempered 6 h at 675 °C (1250 °F). Source: Ref 27
More
Image
Published: 01 June 2024
Fig. 25 Stress-rupture failure of an INCO 713C stress-rupture test bar that was loaded at 414 MPa (60,000 psi) and 816 °C (1500 °F) for 120 h. Thin-film oxidation of the fracture due to elevated-temperature exposure to air is apparent as the iridescent colors. The gradient in fracture surface
More
Image
Published: 01 January 2002
Fig. 6 Logarithmic plot of stress-rupture stress versus rupture life for Co-Cr-Ni-base alloy S-590. The significance of inflection points A, B, N, O, and Y is explained in the text. Source: Ref 10
More
Image
Published: 01 January 2002
Fig. 12 Logarithmic plot of stress-rupture stress versus rupture life for nickel-base alloy U-700 at 815 °C (1500 °F). The increasing slope of the curve to the right of the sigma break is caused by sigma-phase formation.
More
Image
Published: 15 January 2021
Fig. 7 Logarithmic plot of stress-rupture stress versus rupture life for Co-Cr-Ni-base alloy S-590. The significance of inflection points A , B , N , O , and Y is explained in the text. Source: Ref 18
More
Image
Published: 15 January 2021
Fig. 15 Logarithmic plot of stress-rupture stress versus rupture life for nickel-base alloy U-700 at 815 °C (1500 °F). The increasing slope of the curve to the right of the sigma break is caused by sigma-phase formation.
More
Image
Published: 01 June 2016
Fig. 4 Stress-rupture curves for a 1000 h rupture life of selected nickel-base cast superalloys
More
Image
Published: 01 January 2002
Fig. 10 Stress rupture of heater tube. (a) Heater tube that failed due to stress rupture. (b) and (c) Stress-rupture voids near the fracture. Source Ref 10
More
Image
in Properties of Pure Metals
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 62 Stress-rupture life of magnesium as a function of stress and temperature. Source: Ref 208
More
Image
in Service Lifetime Assessment of Polymeric Products
> Characterization and Failure Analysis of Plastics
Published: 15 May 2022
Fig. 8 Stress rupture test showing regression of strength with time and stress in a particular environment
More
Image
Published: 15 January 2021
Fig. 13 (a) Heater tube that failed due to stress rupture. (b) and (c) Stress-rupture voids near the fracture. Source: Ref 18
More
Image
Published: 31 August 2017
Fig. 44 Stress at 0.1% creep strain and stress rupture strength as a function of the Larson-Miller parameter for a 75 mm (3 in.) diameter gray iron rod. Source: Ref 70
More
Image
Published: 01 January 1997
Fig. 17 Stress-rupture behavior of Astroloy. (a) Stress versus time curves. (b) Larson-Miller plot. Source: Ref 69
More
Image
Published: 01 January 1987
Fig. 1267 Fracture of metal-matrix composite stress-rupture specimen. Matrix alloy and processing same as in Fig. 1265 and 1266 . Reinforcing fibers, however, were W-1ThO 2 , 0.5 mm (0.02 in.) in diameter. Specimen failed after 17.5 h at 1095 °C (2000 °F) and 241 MPa (35 ksi). Necking
More
Image
Published: 01 January 1987
Fig. 1268 Fracture of metal-matrix composite stress-rupture specimen. Material and processing same as in Fig. 1265 and 1266 . The composite failed after 3 h at 1205 °C (2200 °F) and 103 MPa (15 ksi). Fibers failed in a brittle mode. Compare with Fig. 1267 . Murakami's reagent, 100× (D.W
More
Image
Published: 01 January 2002
Fig. 1 Micrograph showing stress-rupture cracking at the root of a longitudinal mill defect in a stainless steel superheated tube. The tube ruptured after 18 years of service. Approximately 25×
More
Image
Published: 01 January 2002
Fig. 8 Schematic creep curves for alloys having low and high stress-rupture ductility, showing the increased safety margin provided by the alloy with high stress-rupture ductility. Source: Ref 10
More
1