| タイトル | Aerodynamic characteristics of a 60 degree swept delta-wing space shuttle orbiter at Mach numbers of 2.50, 3.90, and 4.60 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720018347 |
| 著者（英） | Graves, E. B. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1972-05-01 |
| 言語 | eng |
| 内容記述 | Wind tunnel tests were performed to determine the static aerodynamic characteristics of a model of a 60 degree swept delta wing space shuttle orbiter. Some control effectiveness tests were included. The tests were conducted in a unitary plan wind tunnel at Mach numbers of 2.50, 3.90, and 4.60. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 72N25997
L-8243
NASA-TM-X-2561 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203237 |
