| contributor author | David T. Read | |
| contributor author | James W. Dally | |
| date accessioned | 2017-05-08T23:46:55Z | |
| date available | 2017-05-08T23:46:55Z | |
| date copyright | March, 1995 | |
| date issued | 1995 | |
| identifier issn | 1528-9044 | |
| identifier other | JEPAE4-26147#1_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/115169 | |
| description abstract | Fatigue life as a function of number of stress cycles has been determined for three-layer titanium-aluminum-titanium thin-film specimens. For nominal stresses ranging from 50 to 90 percent of the upper-bound ultimate strength, the fatigue lives ranged up to 76 cycles. In all specimens, active cracks were observed after only a few stress cycles. These cracks grew with repeated cycling. The fatigue life was reached when the specimen could no longer sustain the maximum cyclic stress. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Fatigue of Microlithographically-Patterned Free-Standing Aluminum Thin Film Under Axial Stresses | |
| type | Journal Paper | |
| journal volume | 117 | |
| journal issue | 1 | |
| journal title | Journal of Electronic Packaging | |
| identifier doi | 10.1115/1.2792062 | |
| journal fristpage | 1 | |
| journal lastpage | 6 | |
| identifier eissn | 1043-7398 | |
| keywords | Thin films | |
| keywords | Fatigue | |
| keywords | Aluminum | |
| keywords | Stress | |
| keywords | Cycles | |
| keywords | Fatigue life | |
| keywords | Titanium | |
| keywords | Fracture (Materials) AND Tensile strength | |
| tree | Journal of Electronic Packaging:;1995:;volume( 117 ):;issue: 001 | |
| contenttype | Fulltext | |
