| contributor author | G. R. Yoder | |
| contributor author | C. A. Griffis | |
| contributor author | T. W. Crooker | |
| date accessioned | 2017-05-09T01:38:10Z | |
| date available | 2017-05-09T01:38:10Z | |
| date copyright | October, 1974 | |
| date issued | 1974 | |
| identifier issn | 0094-4289 | |
| identifier other | JEMTA8-26838#268_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/164790 | |
| description abstract | This study reveals that degradation in load-carrying capacity owing to sustained-load cracking (SLC) can occur in alloys of the Ti-6Al-4V family. Each of eight alloys tested with fatigue-precracked specimens in ambient room air exhibited the phenomenon, with degradations ranging from 11 to 35 percent. The degree of susceptibility to SLC was seen to be dependent upon crack orientation in rolled plate materials. The threshold stress-intensity factor below which SLC failures will not occur in these alloys, KIt , appears to represent a more conservative fracture-safe design parameter than the plane-strain fracture toughness KIc , which cannot account for time-delayed failures owing to SLC. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Cracking of Ti-6Al-4V Alloys Under Sustained Load in Ambient Air | |
| type | Journal Paper | |
| journal volume | 96 | |
| journal issue | 4 | |
| journal title | Journal of Engineering Materials and Technology | |
| identifier doi | 10.1115/1.3443241 | |
| journal fristpage | 268 | |
| journal lastpage | 274 | |
| identifier eissn | 1528-8889 | |
| keywords | Alloys | |
| keywords | Stress | |
| keywords | Fracture (Process) | |
| keywords | Failure | |
| keywords | Fracture toughness | |
| keywords | Indium alloys | |
| keywords | Plane strain | |
| keywords | Load bearing capacity | |
| keywords | Design AND Fatigue | |
| tree | Journal of Engineering Materials and Technology:;1974:;volume( 096 ):;issue: 004 | |
| contenttype | Fulltext | |
