| タイトル | Model and boundary aerodynamic data from high blockage two-dimensional airfoil tests in a shallow unstreamlined transonic flexible walled test section |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810012558 |
| 著者（英） | Goodyer, M. J.; Wolf, S. W. D. |
| 著者所属（英） | Southampton Univ. |
| 発行日 | 1981-04-01 |
| 言語 | eng |
| 内容記述 | Data for a NACA 0012-64 airfoil at Mach numbers of 0.3, 0.5, and 0.7 with the test section flexible walls set in the "straight" position are presented because they may prove useful in the development of wind tunnel correction techniques. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 81N21087
NASA-CR-165685 |
| 権利 | No Copyright |
