| タイトル | Numerical simulation of a hovering rotor using embedded grids |
| 著者（英） | Duque, Earl-Peter N.; Srinivasan, Ganapathi R. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1992-01-01
1992 |
| 言語 | eng |
| 内容記述 | The flow field for a rotor blade in hover was computed by numerically solving the compressible thin-layer Navier-Stokes equations on embedded grids. In this work, three embedded grids were used to discretize the flow field - one for the rotor blade and two to convect the rotor wake. The computations were performed at two hovering test conditions, for a two-bladed rectangular rotor of aspect ratio six. The results compare fairly with experiment and illustrates the use of embedded grids in solving helicopter type flow fields. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 93A35936 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/317955 |
