| タイトル | Characteristic boundary conditions for three-dimensional transonic unsteady aerodynamics |
| 本文（外部サイト） | http://hdl.handle.net/2060/19850002607 |
| 著者（英） | Whitlow, W., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1984-10-01 |
| 言語 | eng |
| 内容記述 | Characteristic far-field boundary conditions for the three-dimensional unsteady transonic small disturbance potential equation have been developed. The boundary conditions were implemented in the XTRAN3S finite difference code and tested for a flat plate rectangular wing with a pulse in angle of attack; the freestream Mach number was 0.85. The calculated force response shows that the characteristic boundary conditions reduce disturbances that are reflected from the computational boundaries. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 85N10915
NASA-TM-86292
NAS 1.15:86292 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/158059 |
