DocumentCode :
2946849
Title :
A laser fluorescence anemometer for water tunnel flowfield studies
Author :
Owen, F. Kevin
Author_Institution :
Complere Inc., Palo Alto, CA, USA
fYear :
1989
fDate :
18-21 Sep 1989
Firstpage :
298
Lastpage :
309
Abstract :
Successful proof-of-concept experiments carried out using the laser fluorescence anemometer (LFA) in the NASA Ames-Dryden water tunnel are described. The instrument provides for flow visualization and the nonperturbing simultaneous measurement of instantaneous velocity and dye concentration in complex mixing flowfields. The instrument was used in experimental studies of vortex flowfields designed to determine the mechanisms and feasibility of controlling vortex breakdown by introducing relatively low rates of jet blowing along the vortex core. Measurements show that the LFA can provide new insight into the structure, entrainment, and control of mixing vertical and shear layer flows. It is shown that vortex breakdown can be controlled and eliminated by relatively small amounts of jet blowing along the vortex axis
Keywords :
aerospace test facilities; anemometers; flow visualisation; jets; laser velocimeters; vortices; NASA Ames-Dryden water tunnel; aerospace testing; complex mixing flowfields; dye concentration; flow visualization; instantaneous velocity; jet; laser fluorescence anemometer; shear layer flows; vortex breakdown; vortex flowfields; Aerodynamics; Electric breakdown; Fluid flow measurement; Fluorescence; Instruments; Optical mixing; Optical vortices; Spirals; Testing; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1989. ICIASF '89 Record., International Congress on
Conference_Location :
Gottingen
Type :
conf
DOI :
10.1109/ICIASF.1989.77683
Filename :
77683
Link To Document :
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