タイトル | Supersonic Flow Field Investigation Using a Fiber-optic based Doppler Global Velocimeter |
本文(外部サイト) | http://hdl.handle.net/2060/20060023983 |
著者(英) | Cavone, Angelo A.; Fletcher, Mark T.; Lee, Joseph W.; AscencionGuerreroViramontes, J.; Meyers, James F. |
著者所属(英) | NASA Langley Research Center |
発行日 | 2006-05-01 |
言語 | eng |
内容記述 | A three-component fiber-optic based Doppler Global Velocimeter was constructed, evaluated and used to measure shock structures about a low-sonic boom model in a Mach 2 flow. The system was designed to have maximum flexibility in its ability to measure flows with restricted optical access and in various facilities. System layout is described along with techniques developed for production supersonic testing. System evaluation in the Unitary Plan Wind Tunnel showed a common acceptance angle of f4 among the three views with velocity measurement resolutions comparable with free-space systems. Flow field measurements of shock structures above a flat plate with an attached ellipsoid-cylinder store and a low-sonic boom model are presented to demonstrate the capabilities of the system during production testing. |
NASA分類 | Fluid Mechanics and Thermodynamics |
レポートNO | Paper -1019 |
権利 | Copyright, Distribution as joint owner in the copyright |