| contributor author | Chung-Hua Wu | |
| contributor author | Baoguo Wang | |
| date accessioned | 2017-05-08T23:17:51Z | |
| date available | 2017-05-08T23:17:51Z | |
| date copyright | April, 1984 | |
| date issued | 1984 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26604#449_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/98450 | |
| description abstract | The basic aerothermodynamic equations of turbomachine flow expressed with respect to nonorthogonal curvilinear coordinates and corresponding nonorthogonal velocity components are used to solve the compressible flow S1 surface in a turbomachine blade row with splitter vanes or tandem blades. The equation of stream function is solved by matrix technique, and the mass flow ratio and outlet flow angle are determined by applying the Kutta-Joukowsky condition to the trailing edges of the main blade and the splitter vane. Typical examples are given to illustrate the effectiveness of the present method. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Matrix Solution of Compressible Flow on S1 Surface Through a Turbomachine Blade Row With Splitter Vanes or Tandem Blades | |
| type | Journal Paper | |
| journal volume | 106 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239587 | |
| journal fristpage | 449 | |
| journal lastpage | 454 | |
| identifier eissn | 0742-4795 | |
| keywords | Blades | |
| keywords | Compressible flow | |
| keywords | Turbomachinery | |
| keywords | Flow (Dynamics) AND Equations | |
| tree | Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002 | |
| contenttype | Fulltext | |
