| タイトル | Application of the TranAir full-potential code to complete configurations |
| 著者（英） | Erickson, L. L.; Woo, A. C.; Madson, M. D. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | The TranAir computer code solves the full-potential equation for transonic flow by combining a rectangular box of flow-field grid points with networks of surface panels. Complex geometry is easily represented since surface conforming flow-field grids are not used. Application of TranAir to the F-16A is presented for free-stream Mach numbers of 0.6 and 0.90, at an angle of attack of four degrees. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 86A49009 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/382930 |
