| タイトル | Insights into Airframe Aerodynamics and Rotor-on-Wing Interactions from a 0.25-Scale Tiltrotor Wind Tunnel Model |
| 著者（英） | Young, L. A.; Yamauchi, G. K.; McCluer, M.; Derby, M. R.; Lillie, D. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2001-01-01 |
| 言語 | eng |
| 内容記述 | A recent experimental investigation into tiltrotor aerodynamics and acoustics has resulted in the acquisition of a set of data related to tiltrotor airframe aerodynamics and rotor and wing interactional aerodynamics. This work was conducted in the National Full-scale Aerodynamics Complex's (NFAC) 40-by-80 Foot Wind Tunnel, at NASA Ames Research Center, on the Full-Span Tilt Rotor Aeroacoustic Model (TRAM). The full-span TRAM wind tunnel test stand is nominally based on a quarter-scale representation of the V-22 aircraft. The data acquired will enable the refinement of analytical tools for the prediction of tiltrotor aeromechanics and aeroacoustics. |
| NASA分類 | Aircraft Design, Testing and Performance |
| 権利 | Copyright |
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