| タイトル | The direct-stress fatigue strength of 17S-T aluminum alloy throughout the range from 1/2 to 500,000,000 cycles of stress |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930081626 |
| 著者（英） | Hartmann, E C; Stickley, G W |
| 著者所属（英） | National Advisory Committee for Aeronautics |
| 発行日 | 1942-09-01 |
| 言語 | eng |
| 内容記述 | Fatigue-test were conducted on six specimens made from 3/4-inch-diameter 17S-T rolled-and-drawn rod for the purpose of obtaining additional data on the fatigue life of the material at stresses up to the static strength. The specimens were tested in direct tension using a stress range from zero to a maximum in tension. A static testing machine was used to apply repeated loads in the case of the first three specimens; the other three specimens were tested in a direct tension-compression fatigue machine. The direct-stress fatigue curve obtained for the material indicates that, in the range of stresses above about two-thirds the tensile strength, the fatigue strength is higher than might be expected by simply extrapolating the ordinary curve of stress plotted against the number of cycles determined at lower stresses. |
| レポートNO | 93R10916
NACA-TN-865 |
| 権利 | No Copyright |
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