| タイトル | Main rotor free wake geometry effects on blade air loads and response for helicopters in steady maneuvers. Volume 1: Theoretical formulation and analysis of results |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720025345 |
| 著者（英） | Sadler, S. G. |
| 著者所属（英） | Rochester Applied Science Associates, Inc. |
| 発行日 | 1972-09-01 |
| 言語 | eng |
| 内容記述 | A mathematical model and computer program were implemented to study the main rotor free wake geometry effects on helicopter rotor blade air loads and response in steady maneuvers. The theoretical formulation and analysis of results are presented. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 72N32995
NASA-CR-2110
RASA-71-13-VOL-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/202295 |
