| contributor author | M. F. Rothman | |
| contributor author | S. K. Srivastava | |
| date accessioned | 2017-05-08T23:41:24Z | |
| date available | 2017-05-08T23:41:24Z | |
| date copyright | January, 1993 | |
| date issued | 1993 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26712#160_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111977 | |
| description abstract | HAYNES® alloy 242 is a promising new Ni-Mo-Cr alloy for high-strength, high-temperature aerospace fastener applications. Age-hardenable by virtue of a long-range-order strengthening mechanism, 242™ alloy is capable of developing very high strength, particularly in the cold-worked condition. A key difference from other fastener materials is its attendant good ductility. The relationship between the amount of cold work, aging temperature and time, and the properties of this alloy has not been previously explored in detail. In the present work, the nature of the interaction between cold work and aging will be examined, and the properties of the material relevant to aerospace fastener applications will be described. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of Cold Work and Aging Upon the Properties of a Ni-Mo-Cr Fastener Alloy | |
| type | Journal Paper | |
| journal volume | 115 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906671 | |
| journal fristpage | 160 | |
| journal lastpage | 164 | |
| identifier eissn | 0742-4795 | |
| keywords | Alloys | |
| keywords | Fasteners | |
| keywords | Aerospace industry | |
| keywords | High temperature | |
| keywords | Mechanisms | |
| keywords | Ductility AND Temperature | |
| tree | Journal of Engineering for Gas Turbines and Power:;1993:;volume( 115 ):;issue: 001 | |
| contenttype | Fulltext | |
