Variation of properties throughout cross section of two extruded shapes /
Tensile and and compressive properties were determined of specimens cut from the fins and the main bodies of two different extruded shaps of 24S-T aluminum alloy. The specimens from the fins as compared with those from the main body of the section showed: tensile strengths from 5,000 to 10,000 pound...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1941
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
826 |
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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 826 |
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