| タイトル | Transonic cryogenic test section for the Goettingen tube facility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19840008151 |
| 著者（英） | Hornung, H.; Hefer, G.; Krogmann, P.; Stanewsky, E. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1983-12-01 |
| 言語 | eng |
| 内容記述 | The design of modern aircraft requires the solution of problems related to transonic flow at high Reynolds numbers. To investigate these problems experimentally, it is proposed to extend the Ludwieg tube facility by adding a transonic cryogenic test section. After stating the requirements for such a test section, the technical concept is briefly explained and a preliminary estimate of the costs is given. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 84N16219
NASA-TM-77050
NAS 1.15:77050 |
| 権利 | No Copyright |
