| タイトル | Development of a Large Field-of-View PIV System for Rotorcraft Testing in the 14- x 22-Foot Subsonic Tunnel |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090022378 |
| 著者（英） | Bartram, Scott M.; Yao, Chung-Sheng; Mace, W. Derry; Jenkins, Luther N.; Harris, Jerome; Wong, Oliver; Allan, Brian |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2009-05-27 |
| 言語 | eng |
| 内容記述 | A Large Field-of-View Particle Image Velocimetry (LFPIV) system has been developed for rotor wake diagnostics in the 14-by 22-Foot Subsonic Tunnel. The system has been used to measure three components of velocity in a plane as large as 1.524 meters by 0.914 meters in both forward flight and hover tests. Overall, the system performance has exceeded design expectations in terms of accuracy and efficiency. Measurements synchronized with the rotor position during forward flight and hover tests have shown that the system is able to capture the complex interaction of the body and rotor wakes as well as basic details of the blade tip vortex at several wake ages. Measurements obtained with traditional techniques such as multi-hole pressure probes, Laser Doppler Velocimetry (LDV), and 2D Particle Image Velocimetry (PIV) show good agreement with LFPIV measurements. |
| NASA分類 | Aerodynamics |
| レポートNO | LF99-7824 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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