| タイトル | Aeroelastic Stability and Response of Rotating Structures |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040008268 |
| 著者（英） | Keith, Theo G., Jr.; Reddy, Tondapu |
| 著者所属（英） | Toledo Univ. |
| 発行日 | 2004-01-01 |
| 言語 | eng |
| 内容記述 | A summary of the work performed under NASA grant is presented. More details can be found in the cited references. This grant led to the development of relatively faster aeroelastic analysis methods for predicting flutter and forced response in fans, compressors, and turbines using computational fluid dynamic (CFD) methods. These methods are based on linearized two- and three-dimensional, unsteady, nonlinear aerodynamic equations. During the period of the grant, aeroelastic analysis that includes the effects of uncertainties in the design variables has also been developed. |
| NASA分類 | Numerical Analysis |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/89548 |
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