| タイトル | Experimental Results from the Active Aeroelastic Wing Wind Tunnel Test Program |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050203672 |
| 著者（英） | Silva, Walter A.; Lively, Peter; Wieseman, Carol D.; Ivanco, Thomas G.; DeMoss, Joshua; Florance, James R.; Panetta, Andrew; Spain, Charles V.; Tumwa, Vic; Heeg, Jennifer |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2005-01-01 |
| 言語 | eng |
| 内容記述 | The Active Aeroelastic Wing (AAW) program is a cooperative effort among NASA, the Air Force Research Laboratory and the Boeing Company, encompassing flight testing, wind tunnel testing and analyses. The objective of the AAW program is to investigate the improvements that can be realized by exploiting aeroelastic characteristics, rather than viewing them as a detriment to vehicle performance and stability. To meet this objective, a wind tunnel model was crafted to duplicate the static aeroelastic behavior of the AAW flight vehicle. The model was tested in the NASA Langley Transonic Dynamics Tunnel in July and August 2004. The wind tunnel investigation served the program goal in three ways. First, the wind tunnel provided a benchmark for comparison with the flight vehicle and various levels of theoretical analyses. Second, it provided detailed insight highlighting the effects of individual parameters upon the aeroelastic response of the AAW vehicle. This parameter identification can then be used for future aeroelastic vehicle design guidance. Third, it provided data to validate scaling laws and their applicability with respect to statically scaled aeroelastic models. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AIAA Paper 2005-2234 |
| 権利 | No Copyright |
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