Improvement of fatigue life of an aluminum alloy by overstressing /
Fatigue tests were made on some 1.375-inch-diameter and 0.300-incgh diameter specimens of a 17S-T aluminum-alloy rod. One test of a large specimen was run continuously to failure at a maximum stress of 22,000 pounds per square inch. The same nominal maximum stress of 22,000 pounds per square inch wa...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1942
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
857 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 857 |
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