The Effect of Temperature Upon the Fatigue-crack Propagation Behavior of Inconel 625
Author : Lee A. James
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Page : 22 pages
File Size : 33,29 MB
Release : 1977
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Author : Lee A. James
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Page : 22 pages
File Size : 33,29 MB
Release : 1977
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Page : pages
File Size : 24,73 MB
Release : 1977
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The techniques of linear-elastic fracture mechanics were employed to characterize the effect of temperature upon the fatigue-crack propagation behavior of mill-annealed Inconel 625 in an air environment over the range 75/sup 0/- 1200/sup 0/F (24/sup 0/ - 649/sup 0/C). In general, fatigue-crack growth rates increased with increasing test temperature. Two different specimen sizes were employed at each test temperature, and no effects of specimen size upon crack growth were noted.
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Page : 11 pages
File Size : 44,91 MB
Release : 1990
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Fatigue crack propagation of annealed Alloy 625 was studied in air at 24--649 C. Crack growth rates tend to increase with temperature. Two heats were studied; differences in behavior between them suggest a heat-to-heat variability. Characterization of stress ratio (R=K{sub min}/K{sub max}) effects was also done at 538 C.
Author : Lee A. James
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Page : 17 pages
File Size : 42,20 MB
Release : 1976
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Page : pages
File Size : 10,21 MB
Release : 1976
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The techniques of linear-elastic fracture mechanics were employed to characterize the effect of temperature upon the fatigue-crack propagation behavior of precipitation heat-treated Inconel X-750 in an air environment over the range 75-1200/sup 0/F. In general, fatigue-crack growth rates increased with increasing test temperature.
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Page : 1162 pages
File Size : 16,22 MB
Release : 1986
Category : Aeronautics
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Author : Jung Bahadur Singh
Publisher : Springer Nature
Page : 369 pages
File Size : 40,32 MB
Release : 2022-06-29
Category : Technology & Engineering
ISBN : 9811915628
This book gives a brief history of the development of Alloy 625 and a detailed account of its physical, mechanical, and corrosion properties. It also addresses different types of microstructural changes the Alloy 625 undergoes at intermediate temperatures; provides details of properties deterioration due to such microstructural changes; assesses the alloy damage during the in-service inspection of plants; and provides criteria for the damage evaluation for various destructive and non-destructive testing. It combines the industrial data and literature together in one place for damage assessment of service exposed Alloy 625 components. This book serves as a guide to practicing engineers in the industry interested in the use of Alloy 625 and in academia for students pursuing advanced courses in materials science. Alloy 625 is a versatile nickel-chromium-molybdenum alloy known for its unique combination of high strength, excellent fabricability and weldability, and outstanding corrosion resistance.
Author : United States. Energy Research and Development Administration
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Page : 900 pages
File Size : 45,38 MB
Release : 1977
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Author : United States. Energy Research and Development Administration. Technical Information Center
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Page : 1066 pages
File Size : 18,4 MB
Release : 1977
Category : Force and energy
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Page : 18 pages
File Size : 21,55 MB
Release : 1976
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