• 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