| タイトル | The 40 X 80 X 120 Wind Tunnel Project |
| 本文（外部サイト） | http://hdl.handle.net/2060/19920075365 |
| 著者（英） | Falarski, Michael D. |
| 発行日 | 1984-03-20 |
| 言語 | eng |
| 内容記述 | The scope of this project includes increasing the speed of the 40 x 80 x 120 foot closed circuit wind tunnel to 300 knots to expand rotorcraft research capability, and to add an 80 x 120 foot open circuit wind tunnel with 100 knot maximum speed to expand vertical supersonic takeoff and landing research and capability. Topics discussed in viewgraph format are: wind tunnel characteristics, a cost analysis, and design of wind tunnel models. |
| NASA分類 | Research and Support Facilities (Air); Aerodynamics |
| レポートNO | 92N70489 |
| 権利 | Copyright, Public use permitted |
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