| タイトル | An evaluation of aerodynamics modeling of spinning light airplanes |
| 著者（英） | Taylor, L. W., Jr.; Pamadi, B. N. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1983-01-01 |
| 言語 | eng |
| 内容記述 | This paper extends the application of the modified strip theory for wing body combination of a spinning light airplane reported earlier. In addition, to account for the contribution of the tail plane, the shielding effect on vertical tail under steady state spin condition is modeled from basic aerodynamic considerations. The results of this combined analysis, presented for some light airplane configurations, are shown to be in good agreement with spin tunnel rotary balance test data. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 83A17922
AIAA PAPER 83-0368 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/405981 |
