| タイトル | Transonic Wind-Tunnel Test Of An Oblique Wing |
| 著者（英） | Carmichael, R. L.; Strong, J. M.; Kroo, I. M.; Kennelly, R. A. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1992-12-01 |
| 言語 | eng |
| 内容記述 | Report describes transonic wind-tunnel tests of oblique, pivotable wing fitted to 0.087-scale model of F-8 airplane. Purpose of tests to study performance and stability characteristics. Conducted to determine whether placement of pivot at higher position above fuselage than previously results in less side force and yawing moment than observed in previous tests at low speeds. |
| NASA分類 | MECHANICS |
| レポートNO | 92B10759
ARC-12812 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/331760 |
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