| タイトル | Model equations for simulating flows in multistage turbomachinery |
| 著者（英） | Adamczyk, John J. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1996-01-01
1996 |
| 言語 | eng |
| 内容記述 | A steady, three dimensional average-passage equation system was derived. The purpose was to simulate multistage turbomachinery flows. These equations describe a steady, viscous flow that is periodic from blade passage to blade passage. Moreover, these equations have a closure problem that is similar to that of the Reynolds-average Navier-Stokes equations. A scaled form of the average-passage equation system could provide an improved mathematical model for simulating the flow in the design and in the off-design conditions of a multistage machine. |
| NASA分類 | Fluid Mechanics and Heat Transfer |
| レポートNO | 97N10711 |
| 権利 | Copyright, Distribution within the U.S. granted by agreement |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/518747 |
