| タイトル | Development of the cryogenic tunnel concept and application to the US National Transonic Facility |
| 著者（英） | Kilgore, R. A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1979-11-01 |
| 言語 | eng |
| 内容記述 | A fan-driven, high Reynolds number, transonic cryogenic wind tunnel is described. The tunnel has a 2.5- by 2.5 m test section and is capable of operating from ambient to cryogenic temperatures at stagnation pressures up to 8.8 atm. An overview of the cryogenic concept and discussions of drive power requirements, support systems, and operating characteristics and performance of the wind tunnel are included. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 80N19139 |
| 権利 | Copyright, Distribution within the U.S. granted by agreement |
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