| タイトル | Simulation of three-dimensional viscous flow within a multistage turbine |
| 著者（英） | Barnett, Mark; Adamczyk, John J.; Celestina, Mark L.; Beach, Tim A. |
| 著者所属（英） | Sverdrup Technology, Inc.; NASA Lewis Research Center; United Technologies Research Center |
| 発行日 | 1989-06-01 |
| 言語 | eng |
| 内容記述 | This work outlines a procedure for simulating the flow field within multistage turbomachinery which includes the effects of unsteadiness, compressibility, and viscosity. The associated modeling equations are the average passage equation system which governs the time-averaged flow field within a typical passage of a blade row embedded within a multistage configuration. The results from a simulation of a low aspect ratio stage and a one-half turbine will be presented and compared with experimental measurements. It will be shown that the secondary flow field generated by the rotor causes the aerodynamic performance of the downstream vane to be significantly different from that of an isolated blade row. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 90A23841
ASME PAPER 89-GT-152 |
| 権利 | Copyright |
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