The direct-stress fatigue strength of 17S-T aluminum alloy throughout the range from 1/2 to 500,000,000 cycles of stress / by E.C. Hartmann and G.W. Stickley.
Saved in:
| Online Access: |
Online Access |
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| Main Authors: | , |
| Format: | Government Document eBook |
| 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) ;
865. |
| Subjects: |
Internet
Online AccessOnline
| Call Number: |
Y 3.N 21/5:6/865
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| Y 3.N 21/5:6/865 | Available |