| contributor author | E. R. McFarland | |
| date accessioned | 2017-05-08T23:17:50Z | |
| date available | 2017-05-08T23:17:50Z | |
| date copyright | April, 1984 | |
| date issued | 1984 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26604#376_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/98440 | |
| description abstract | A rapid technique for solving the blade-to-blade turbomachinery flow problem has been developed. Approximate governing flow equations, which include the effects of compressibility, radius change, rotation, and variable stream sheet thickness are solved using an improved panel method. The development and solution of these equations are described. Sample calculations are presented to illustrate the method’s capabilities and accuracy. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Rapid Blade-to-Blade Solution for Use in Turbomachinery Design | |
| type | Journal Paper | |
| journal volume | 106 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239574 | |
| journal fristpage | 376 | |
| journal lastpage | 382 | |
| identifier eissn | 0742-4795 | |
| keywords | Design | |
| keywords | Blades | |
| keywords | Turbomachinery | |
| keywords | Flow (Dynamics) | |
| keywords | Equations | |
| keywords | Thickness | |
| keywords | Rotation AND Compressibility | |
| tree | Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002 | |
| contenttype | Fulltext | |
