| タイトル | The computation of flow past an oblique wing using the thin-layer Navier-Stokes equations |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880020390 |
| 著者（英） | Mehta, Unmeel |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1986-06-01 |
| 言語 | eng |
| 内容記述 | Essential aspects are presented for computing flow past an oblique wing with the thin-layer Navier-Stokes equations. A new method is developed for generating a grid system around a realistic wing. This method utilizes a series of conformal transformations. The thin-shear-layer approximation and an algebraic eddy-viscosity turbulence model are used to simplify the Reynolds-averaged Navier-Stokes equations. An implicit, factored numerical scheme and the concept of pencil data structure are utilized. For the first time, some flow fields caused by the oblique wing in a supersonic free stream are discussed, emphasizing the separated vortex flows associated with such a wing. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88N29774
NAS 1.15:88317
A-86295
NASA-TM-88317 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/145395 |
