The direct-stress fatigue strength of 17S-T aluminum alloy throughout the range from 1/2 to 500,000,000 cycles of stress
| Author: | Hartmann, E C |
|---|---|
| Year: | 1942 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-865 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54720/ |