| contributor author | R. B. Deshpande | |
| date accessioned | 2017-05-08T22:58:53Z | |
| date available | 2017-05-08T22:58:53Z | |
| date copyright | September, 1975 | |
| date issued | 1975 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26873#372_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/87634 | |
| description abstract | A new algorithm, which is a modification of the successive over-relaxation method, has been applied to the inviscid compressible blade-to-blade flow problem. When this procedure was used, an improvement in convergence of the numerical process was obtained with a reduction of computing time by a factor of 2. This technique offers another advantage of obtaining convergence where other methods might have been unsuccessful. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A New Algorithm for the Solution of Turbomachinery Flow Problems | |
| type | Journal Paper | |
| journal volume | 97 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3447317 | |
| journal fristpage | 372 | |
| journal lastpage | 374 | |
| identifier eissn | 1528-901X | |
| keywords | Flow (Dynamics) | |
| keywords | Algorithms | |
| keywords | Turbomachinery | |
| keywords | Blades AND Relaxation (Physics) | |
| tree | Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 003 | |
| contenttype | Fulltext | |
