| タイトル | Computational/experimental study of the flowfield on a body of revolution at incidence |
| 著者（英） | Zilliac, G. G. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1989-08-01 |
| 言語 | eng |
| 内容記述 | A joint computational-experimental study of the vortical flowfield on a pointed body of revolution is undertaken. The incompressible Navier-Stokes equations are solved numerically for steady flow around an ogive-cylinder at angle of attack. The three-dimensional vortical flow is investigated, with emphasis on the tip and the near-wake region. Comparisons of computational results with results of a companion towing-tank experiment are presented at Re(L) = 1000. Results of a wind tunnel experiment at Re(L) = 820,000, featuring use of a seven-hole pressure probe, also are presented. It was observed that at the low Reynolds number of the towing tank study, the leeside flow was symmetric at the angles of attack considered. For the same configuration at the higher Reynolds number of the wind tunnel study, the flow was asymmetric under equivalenat conditions for some of the angles of attack studied. The topology of the flow is discussed and conclusions are drawn concerning the growth and stability of the primary vortices. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 89A47353
AIAA PAPER 87-2277 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/362160 |
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