| contributor author | C. F. Grainger | |
| date accessioned | 2017-05-08T23:09:03Z | |
| date available | 2017-05-08T23:09:03Z | |
| date copyright | September, 1980 | |
| date issued | 1980 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26962#338_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93465 | |
| description abstract | The three-dimensional flow through a cascade of twisted flat-plate blades is calculated using a computer program based on a finite-difference approximation to the method of characteristics. The relative flow is supersonic but the axial flow is subsonic. For two-dimensional flow under similar conditions, the inlet flow field is one of “unique-incidence,” the effect discussed by Starken (5) and others. The main purpose of the present work is to extend the understanding of this effect to three-dimensional flow. Important differences between the two and three-dimensional flow fields are explained in terms of the interaction between neighboring sections of the flow. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Three Dimensional Supersonic Flow Through a Cascade of Twisted Flat Plates | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3240691 | |
| journal fristpage | 338 | |
| journal lastpage | 343 | |
| identifier eissn | 1528-901X | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Flat plates | |
| keywords | Supersonic flow | |
| keywords | Flow (Dynamics) | |
| keywords | Approximation | |
| keywords | Axial flow | |
| keywords | Blades AND Computer software | |
| tree | Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 003 | |
| contenttype | Fulltext | |
