| タイトル | Experimental Test Of Aerodynamic Computer Program |
| 著者（英） | Madson, M. D.; Erickson, L. L. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1988-02-01 |
| 言語 | eng |
| 内容記述 | Linear potential-flow theory applied to advanced airplane design. Report discusses use of PANAIR computer program to predict airflow about advanced fighter aircraft. Predictions compared with measurements about scale model of aircraft in wind tunnel at mach numbers of 0.6, 0.9, and 1.2 and at angles-of-attack from 0 to 10 degree. |
| NASA分類 | MECHANICS |
| レポートNO | 88B10123
ARC-11733 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/375387 |
