| タイトル | Guide for users of the National Transonic Facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810020601 |
| 著者（英） | Gloss, B. B.; Nystrom, D.; Fuller, D. E. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1981-07-01 |
| 言語 | eng |
| 内容記述 | The National Transonic Facility (NTF) is a fan-driven, closed-circuit, continuous flow, pressurized wind tunnel. The test section is 2.5 m x 2.5 m and 7.62 m long with a slotted-wall configuration. The NTF will have a Mach number range from 0.2 to 1.2, with Reynolds number up to 120 10 to the sixth power at Mach 1 (based on a reference length of 0.25 m). The pressure range for the facility will be from 1 to about 9 bars (1 ban = 100 kPa), and the temperature can be varied from 340 to 78 K. This report provides potential users of the NTF with the information required for preliminary planning to test programs and for preliminary layout of models and model supports which may be used in such programs. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 81N29139
NASA-TM-83124
L-14077 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/168365 |
