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