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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...
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...
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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 More
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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 More
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Published: 01 December 2003
Fig. 7 Typical creep and creep rupture curves for polymers. (a) Ductile polymers. (b) Brittle polymers More
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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 More
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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 More
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Published: 01 December 2008
Fig. 21 100,000-h creep rupture strength More
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Published: 01 November 2007
Fig. 14.32 Creep rupture ductility of alloy 800H as a function of combined Al+Ti content in the alloy tested at 650 °C (1200 °F). Source: Ref 38 More
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Published: 01 December 1989
Fig. 7.21. Loss in creep-rupture life of ½Mo steel at 540 °C (1000 °F) in 5-MPa (725-psi) hydrogen ( Ref 56 ). More
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Published: 01 December 1989
Fig. 7.39. Creep-rupture strength of a low-silicon 2¼Cr-1Mo-¼V-Ti-B developmental steel ( Ref 84 ). More
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Published: 01 December 1989
Fig. 8.15. Comparison of creep-rupture properties of modified 9Cr-1Mo steel weldment and base metal, illustrating effect of type IV cracking ( Ref 54 ). More
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Published: 01 December 1989
Fig. 9.7. Development of new alloys for increased creep-rupture strength ( Ref 3 ). More
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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. More
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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 ). More
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Published: 01 December 1989
Fig. 4.28. Creep-rupture/low-cycle-fatigue damage interaction curve for 1Cr-Mo-V rotor steel at 540 °C (1000 °F) (after Ref 82 ). More
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Published: 01 December 1989
Fig. 5.3. Creep-rupture failures in boiler tubes ( Ref 1 ). (a) Typical short-term overheating failure. (b) Typical long-term creep failure. More
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Published: 01 December 1989
Fig. 5.25. Above: Graph showing results of creep-rupture tests on 1Cr-½Mo steel after removal from boiler tubes (tests at 510 °C, or 950 °F). Below: Micrographs showing stages of spheroidization present in samples at beginning of test ( Ref 45 ). Stage A (top left): Ferrite and very fine More
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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 More
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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 More