| タイトル | Successive smoothing algorithm for constructing the semiempirical model developed at ONERA to predict unsteady aerodynamic forces |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820016298 |
| 著者（英） | Petot, D.; Loiseau, H. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1982-03-01 |
| 言語 | eng |
| 内容記述 | Unsteady aerodynamic methods adopted for the study of aeroelasticity in helicopters are considered with focus on the development of a semiempirical model of unsteady aerodynamic forces acting on an oscillating profile at high incidence. The successive smoothing algorithm described leads to the model's coefficients in a very satisfactory manner. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82N24174
NASA-TM-76681
NAS 1.15:76681 |
| 権利 | No Copyright |
|
