タイトル | A critical evaluation of a three-dimensional Navier-Stokes CFD as a tool to design supersonic turbine stages |
著者(英) | Shoemaker, M.; Hah, C.; Kwon, O. |
著者所属(英) | NASA Lewis Research Center |
発行日 | 1992-07-01 |
言語 | eng |
内容記述 | Three-dimensional flow phenomena in a supersonic turbine blade row were studied numerically to evaluate CFD as a tool to design supersonic turbine stages. The details of the three-dimensional flow structure inside the supersonic turbine blade row and the overall aerodynamic performance at design and off-design conditions are analyzed and the results are compared between the experimental data and the numerical results. |
NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
レポートNO | 92N32268 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/230683 |