| contributor author | R. A. Novak | |
| contributor author | R. M. Hearsey | |
| date accessioned | 2017-05-08T23:03:14Z | |
| date available | 2017-05-08T23:03:14Z | |
| date copyright | March, 1977 | |
| date issued | 1977 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26910#154_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/90098 | |
| description abstract | The structure of a computing system for bladed or unbladed turbomachinery passages is described and discussed. The system, in an overall sense, is modeled after the work of Wu, and is comprised of two coordinated computer programs, one providing solutions on rotationally symmetric blade-to-blade surfaces and the second on streamsheets roughly parallel to the blades. Both approaches utilize streamline curvature techniques. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Nearly Three-Dimensional Intrablade Computing System for Turbomachinery | |
| type | Journal Paper | |
| journal volume | 99 | |
| journal issue | 1 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3448517 | |
| journal fristpage | 154 | |
| journal lastpage | 166 | |
| identifier eissn | 1528-901X | |
| keywords | Turbomachinery | |
| keywords | Blades AND Computer software | |
| tree | Journal of Fluids Engineering:;1977:;volume( 099 ):;issue: 001 | |
| contenttype | Fulltext | |
