| contributor author | T. Q. Dang | |
| date accessioned | 2017-05-08T23:40:00Z | |
| date available | 2017-05-08T23:40:00Z | |
| date copyright | January, 1992 | |
| date issued | 1992 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28617#141_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/111131 | |
| description abstract | The newly developed three-dimensional design technique for turbomachinery blading based on the circulation method has been successfully extended into the transonic flow regime. The main task involves replacing the classical Fourier series expansion technique by a finite-volume method. Calculations were carried out for the design of infinitely thin cascaded blades in transonic flows, including shocked and shock-free cascaded blades. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Design of Turbomachinery Blading in Transonic Flows by the Circulation Method | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927977 | |
| journal fristpage | 141 | |
| journal lastpage | 146 | |
| identifier eissn | 1528-8900 | |
| keywords | Design | |
| keywords | Transonic flow | |
| keywords | Turbomachinery | |
| keywords | Blades | |
| keywords | Finite volume methods | |
| keywords | Fourier series AND Shock (Mechanics) | |
| tree | Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001 | |
| contenttype | Fulltext | |
