| タイトル | Application of TURBO-AE to Flutter Prediction: Aeroelastic Code Development |
| 本文（外部サイト） | http://hdl.handle.net/2060/20010047229 |
| 著者（英） | Hoyniak, Daniel; Stefko, George; Simons, Todd A. |
| 著者所属（英） | Rolls-Royce Allison |
| 発行日 | 2001-05-01 |
| 言語 | eng |
| 内容記述 | The TURBO-AE program has been evaluated by comparing the obtained results to cascade rig data and to prediction made from various in-house programs. A high-speed fan cascade, a turbine cascade, a turbine cascade and a fan geometry that shower flutter in torsion mode were analyzed. The steady predictions for the high-speed fan cascade showed the TURBO-AE predictions to match in-house codes. However, the predictions did not match the measured blade surface data. Other researchers also reported similar disagreement with these data set. Unsteady runs for the fan configuration were not successful using TURBO-AE . |
| NASA分類 | Aerodynamics |
| レポートNO | NASA/CR-2001-210761
EDR-19540
NAS 1.26:210761 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/93063 |
