| contributor author | S. Damle | |
| contributor author | J. Stringham | |
| contributor author | E. Razinsky | |
| contributor author | T. Dang | |
| date accessioned | 2017-05-09T00:01:18Z | |
| date available | 2017-05-09T00:01:18Z | |
| date copyright | April, 1999 | |
| date issued | 1999 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28669#321_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/123043 | |
| description abstract | The practical utility of a three-dimensional inverse viscous method is demonstrated by carrying out a design modification of a first-stage rotor in an industrial compressor. In this design modification study, the goal is to improve the efficiency of the original blade while retaining its overall aerodynamic, structural, and manufacturing characteristics. By employing a simple modification to the blade pressure loading distribution (which is the prescribed flow quantity in this inverse method), the modified blade geometry is predicted to perform better than the original design over a wide range of operating points, including an improvement in choke margin. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Practical Use of Three-Dimensional Inverse Method for Compressor Blade Design | |
| type | Journal Paper | |
| journal volume | 121 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2841317 | |
| journal fristpage | 321 | |
| journal lastpage | 325 | |
| identifier eissn | 1528-8900 | |
| keywords | Compressors | |
| keywords | Design | |
| keywords | Blades | |
| keywords | Geometry | |
| keywords | Rotors | |
| keywords | Manufacturing | |
| keywords | Pressure AND Flow (Dynamics) | |
| tree | Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002 | |
| contenttype | Fulltext | |