| タイトル | Assessment of three-dimensional inviscid codes and loss calculations for turbine aerodynamic computations |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840008074 |
| 著者（英） | Povinelli, L. A. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1984-01-01 |
| 言語 | eng |
| 内容記述 | An assessment of several three dimensional inviscid turbine aerodynamic computer codes and loss models used at the NASA Lewis Research Center is presented. Five flow situations are examined, for which both experimental data and computational results are available. The five flows form a basis for the evaluation of the computational procedures. It was concluded that stator flows may be calculated with a high degree of accuracy, whereas, rotor flow fields are less accurately determined. Exploitation of contouring, learning, bowing, and sweeping will require a three dimensional viscous analysis technique. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 84N16142
E-1951
NASA-TM-83571
NAS 1.15:83571 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/160674 |
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