| contributor author | J. H. Horlock | |
| 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#330_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93464 | |
| description abstract | An actuator disk method is developed for calculating the flow through the blade rows of a turbomachine in which the velocity relative to the blading may be supersonic. The method is compared with calculations of the fully supersonic flow through a twisted blade row using a three-dimensional method of characteristics. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Linearized Solutions for the Supersonic Flow Through Turbomachinery Blade Rows (Using Actuator Disk Theory) | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3240690 | |
| journal fristpage | 330 | |
| journal lastpage | 337 | |
| identifier eissn | 1528-901X | |
| keywords | Actuators | |
| keywords | Disks | |
| keywords | Blades | |
| keywords | Supersonic flow | |
| keywords | Turbomachinery AND Flow (Dynamics) | |
| tree | Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 003 | |
| contenttype | Fulltext | |
