| タイトル | NASA Lewis 8 by 6 foot supersonic wind tunnel |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740017676 |
| 著者（英） | Aiello, R. A.; Swallow, R. J. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1974-05-01 |
| 言語 | eng |
| 内容記述 | Performance data are presented for the tunnel, which has a Mach number range from 0.36 to 2.0. The tunnel circuit, test section, model support systems, auxiliary systems, instrumentation, control room equipment, and automatic recording and computing equipment are also described. Information is presented on criteria for designing models and on shop facilities available to prospective users. |
| NASA分類 | FACILITIES, RESEARCH, AND SUPPORT |
| レポートNO | 74N25789
E-7949
NASA-TM-X-71542 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/194570 |
