| contributor author | George A. Hoffman | |
| date accessioned | 2017-05-09T00:03:29Z | |
| date available | 2017-05-09T00:03:29Z | |
| date copyright | November, 1960 | |
| date issued | 1960 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27441#363_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/124389 | |
| description abstract | A method is derived for specifying economically optimum tolerances for a variety of sheet materials for use in flight vehicles. The results indicate a significant disparity between present industry practices and the apparent optimum tolerances. These tolerances are listed as possible target requirements for rolling programs of new and future metals. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Optimum Tolerances of Sheet Materials for Flight Vehicles | |
| type | Journal Paper | |
| journal volume | 82 | |
| journal issue | 4 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3664246 | |
| journal fristpage | 363 | |
| journal lastpage | 366 | |
| identifier eissn | 1528-8935 | |
| keywords | Vehicles | |
| keywords | Sheet materials | |
| keywords | Flight AND Metals | |
| tree | Journal of Manufacturing Science and Engineering:;1960:;volume( 082 ):;issue: 004 | |
| contenttype | Fulltext | |
