| contributor author | A. Massardo | |
| contributor author | A. Satta | |
| contributor author | M. Marini | |
| date accessioned | 2017-05-08T23:34:05Z | |
| date available | 2017-05-08T23:34:05Z | |
| date copyright | July, 1990 | |
| date issued | 1990 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28604#405_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107728 | |
| description abstract | A new technique is presented for the design optimization of an axial-flow compressor stage. The procedure allows for optimization of the complete radial distribution of the geometry, since the variables chosen to represent the three-dimensional geometry of the stage are coefficients of suitable polynomials. Evaluation of the objective function is obtained with a throughflow calculation, which has acceptable speed and stability qualities. Some examples are given of the possibility to use the procedure both for redesign and, together with what was presented in Part I, for the complete design of axial-flow compressor stages. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Axial Flow Compressor Design Optimization: Part II—Throughflow Analysis | |
| type | Journal Paper | |
| journal volume | 112 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927674 | |
| journal fristpage | 405 | |
| journal lastpage | 410 | |
| identifier eissn | 1528-8900 | |
| keywords | Design | |
| keywords | Optimization | |
| keywords | Axial flow | |
| keywords | Geometry | |
| keywords | Compressors | |
| keywords | Stability AND Polynomials | |
| tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003 | |
| contenttype | Fulltext | |