| タイトル | Fuselage surface pressure measurements of a helicopter wind-tunnel model with a 3.15-meter diameter single rotor |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790017844 |
| 著者（英） | Mineck, R. E.; Freeman, C. E. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1979-03-01 |
| 言語 | eng |
| 内容記述 | A wind-tunnel investigation was conducted to measure the time averaged fuselage surface pressures of a helicopter model with a 3.15 meter diameter, four-bladed articulated rotor. Measurements were made at hover and advance ratios of 0.05, 0.15, and 0.20 for a range of thrusts. Data are presented with no analysis. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 79N26015
NASA-TM-80051 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/175233 |
