The Rate of Fatigue-crack Propagation for Two Aluminum Alloys Under Completely Reversed Loading PDF Download
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Author: Walter Illg
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 24
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Author: Walter Illg
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 24
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Author: Jack Telesman
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
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Author: Arthur J. McEvily
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ISBN:
Category : Aluminum alloys
Languages : en
Pages : 46
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A general method has been developed for the determination of fatigue-crack propagation rates. In order to provide a check on the theoretical predictions and to evaluate certain empirical constants appearing in the expression for the rate of fatigue-crack propagation, an extensive series of tests has been conducted. Sheet specimens, 2 inches and 12 inches wide, of 2024-T3 and 7075-T6 aluminum alloys were tested in repeated tension with constant-amplitude loading. Stresses ranged up to 50 ksi, based on the initial area. Good agreement between the results and predictions was found.
Author: Jack Telesman
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Author: C. M. Hudson
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 36
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Stress ratio effects on fatigue crack growth in sheet aluminum alloys.
Author: Robert G. Dubensky
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 36
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 300
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
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