| タイトル | Finite Element Stability Analysis for Coupled Rotor and Support Systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770019135 |
| 著者（英） | Hohenemser, K. H.; Yin, S. K. |
| 著者所属（英） | Washington Univ. |
| 発行日 | 1977-06-01 |
| 言語 | eng |
| 内容記述 | The effects of fuselage motions on stability and random response were analytically assessed. The feasibility of adequate perturbation models from non-linear trim conditions was studied by computer and hardware experiments. Rotor wake-blade interactions were assessed by using a 4-bladed rotor model with the capability of progressing and regressing blade pitch excitation (cyclic pitch stirring), by using a 4-bladed rotor model with hub tilt stirring, and by testing rotor models in sinusoidal up or side flow. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 77N26079
NASA-CR-152024 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/182044 |
