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creep rupture
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060021
EISBN: 978-1-62708-343-0
... Abstract This chapter focuses on creep-rupture failure, or more precisely, the time required for such a failure to occur at a given stress and temperature. It begins with a review of creep-rupture phenomena and the various ways creep-rupture data are presented and analyzed. It then examines...
Abstract
This chapter focuses on creep-rupture failure, or more precisely, the time required for such a failure to occur at a given stress and temperature. It begins with a review of creep-rupture phenomena and the various ways creep-rupture data are presented and analyzed. It then examines a large collection of creep-rupture data corresponding to different alloy designations and heat treatments, identifying key relationships, similarities, and differences. It also presents a test method developed by the authors in which twelve materials are tested over a range of temperature, stress, and time in order to determine multiheat constants that are then used to fit multiheat data from other materials and thus estimate rupture times.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140243
EISBN: 978-1-62708-335-5
... Abstract This data set contains the results of uniaxial creep rupture tests for a wide range of aluminum casting alloys conducted at temperatures from 100 to 315 deg C. In most cases, tests were made of several lots of material of each alloy and temper, the results were analyzed...
Abstract
This data set contains the results of uniaxial creep rupture tests for a wide range of aluminum casting alloys conducted at temperatures from 100 to 315 deg C. In most cases, tests were made of several lots of material of each alloy and temper, the results were analyzed, and the averages were normalized to the room-temperature typical values. For some alloys, "representative" values (raw data) rather than typical values are provided.
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in Partitioning of Hysteresis Loops and Life Relations
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 5.13 Variation in creep-rupture ductility with creep-rupture failure time. (a) Normalized and tempered 2¼Cr-1Mo steel at 540 °C (1000 °F). (b) Quenched and tempered 2¼Cr-1Mo tested at 485 °C (900 °F). (c) Solution-annealed AISI type 304 stainless steel tested at 650 °C (1200 °F). Source
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Published: 01 March 2002
Fig. 12.79 Average rupture elongation of creep-rupture-tested longitudinal CGDS and PC cast MAR-M-200
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in Mechanical Testing and Properties of Plastics: An Introduction[1]
> Characterization and Failure Analysis of Plastics
Published: 01 December 2003
Fig. 7 Typical creep and creep rupture curves for polymers. (a) Ductile polymers. (b) Brittle polymers
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Published: 01 July 2009
Fig. 1.22 Creep-rate response in tension and compression of a cyclic creep-rupture test of 316 stainless steel (heat 1) at 705 °C (1300 °F). Source: Ref 1.62
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Published: 01 July 2009
Fig. 1.23 Comparison of tensile/compressive creep rates of a cyclic creep-rupture test of 316 stainless steel (heat 2) at 705 °C (1300 °F). Source: Ref 1.62
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Published: 01 October 2011
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Published: 01 October 2011
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Published: 01 October 2011
Fig. 16.15 Fish mouth fracture from creep rupture of a type 321 stainless steel superheater tube
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Published: 01 December 2003
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.14 Creep-rupture properties of conventionally cast (PWA 659), directionally solidified (PWA 664), and single crystal (directionally solidified monocrystaloy) (PWA 1409). Source: Ref 11.18
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Published: 01 March 2002
Fig. 12.51 Creep-rupture behavior of two cobalt-base (MAR-M-302 and WI-52) and two nickel-base (MAR-M-200 and B-1900) superalloys at 982 °C (1800 °F), showing the creep-rupture superiority of nickel-base to cobalt-base superalloys
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Published: 01 March 2002
Fig. 12.71 Comparison of creep-rupture life of IN-792 type SCDS alloy with primary orientation deviations (α) of 10° and 25° using Larson-Miller parameter (P LM ). Note: P LM = T (C + log t ) where C = Larson-Miller constant, T = absolute temperature, t = time in h. For this plot, C
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Published: 01 July 2009
Fig. 1.21 Early concept of cyclic creep-rupture testing (a) Hysteresis loop. (b) Imposed cyclic stress history and cyclic strain response. Source: Ref 1.62
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Published: 01 July 2009
Fig. 2.8 Actual creep-rupture behavior for the eight heats of alloy 21 in Table 2.3 . Scatter appears to be high.
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Published: 01 July 2009
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in Critique of Predictive Methods for Treatment of Time-Dependent Metal Fatigue at High Temperatures
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 8.7 Comparison of static and cyclic creep-rupture curves for L-605 alloy. Source: Ref 8.41
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Published: 01 December 1989
Fig. 1.8. Uncertainty in creep-rupture life assessment due to scatter in the properties of a Cr-Mo-V steel.
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Published: 01 December 1989
Fig. 3.32. Plot of data from accelerated creep-rupture tests on retired header specimens, illustrating the isostress method ( Ref 160 ).
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