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| Title: |
Effect of Fatigue Crack on Static Strength: 2014-T6, 2024-T4, 6061-T6, 7075-T6 Open-Hole Monobloc Specimens
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| Author(s): |
Nordmark, Glenn E.; Eaton, Ian D.
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| Abstract: |
Static tensile test results are presented for specimens of 2014-T6, 2024-T4, 6061-T6, and 7075-T6 aluminum alloy containing fatigue cracks. The results are found to be in good agreement with the results reported for similar tests from other sources. The results indicate that the presence of a fatigue crack reduced the static strength, in all cases, by an amount larger than the corresponding reduction in net area; the 6061-T6 alloy specimens were least susceptible to the crack and the 7075-T6 alloy specimens were most susceptible. It is indicated that a 7075-T6 specimen may develop as little as one-third of the expected static tensile strength when the fatigue crack was consumed only one-fourth of the original area. It was found that the static strength was substantially higher for specimens which had stop holes drilled at the end of the fatigue crack.
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| NASA Center: |
NACA (Unspecified Center)
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| Publication Date: |
May 1957
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| Document Source: |
CASI |
| Online Source: |
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| Document ID: |
20040034248
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| Publication Information: |
Number of Pages = 23 |
| Report Number: |
NACA-TM-1428
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| Price Code: |
A03 |
| Keywords: |
ALUMINUM ALLOYS; CRACKS; TENSILE STRENGTH; STATIC TESTS; TENSILE TESTS; FATIGUE (MATERIALS); HOLES (MECHANICS);
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| Accessibility: |
Unclassified; No Copyright; Unlimited; Publicly available; |
| Updated/Added to NTRS: |
2005-10-13 |
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