Effects of range of stress and of special notches on fatigue properties of aluminum alloys suitable for airplane propellers /
Laboratory tests were made to obtain information on the load-resisting properties of X76S-T aluminum alloy when subjected to static, impact, and repeated loads. Results are presented from static-load tests of notched specimens in tension. Charpy impact values obtained from bend tests on notched spec...
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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) ;
852 |
| 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 852 |
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