• DocumentCode
    1719578
  • Title

    Doppler Global Velocimetry (DGV) data in circular jets

  • Author

    Kuhlman, John ; Burton, Lucinda ; Scarberry, Tom

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., West Virginia Univ., Morgantown, WV, USA
  • fYear
    2001
  • fDate
    8/1/2001 12:00:00 AM
  • Firstpage
    219
  • Lastpage
    230
  • Abstract
    A two-component Doppler Global Velocimeter (DGV) system has been improved through the use of vapor-limited iodine cells that have temperature-independent responses, along with non-polarizing beam splitters and lower f-number lenses. Two-component DGV velocity measurements have been obtained for a 1 inch diameter uniform circular jet flow at a nominal exit velocity of 60 m/sec, as well as for an annular jet and a swirling jet. These data generally agree with earlier point Doppler velocimeter (pDv) and hot wire anemometer results to within about 2-4 m/sec, and display a total variability from a smooth curve of ± 2-3 m/sec. Exceptions to this level of accuracy are noted in regions of significant secondary scattering, due to scattered laser light that is reflected off of the lip of the jet nozzle, as well as in regions of low smoke seeding levels, resulting in a low signal-to-noise ratios. A significant amount of the variability of the data from a smooth curve is due to the flat field correction
  • Keywords
    flow visualisation; jets; laser velocimeters; laser velocimetry; rotational flow; wind tunnels; 60 m/s; Doppler global velocimetry; aerodynamic testing; annular jet; circular jets; complex flow field; flat field correction; nonpolarizing beam splitters; secondary scattering; swirling jet; temperature-independent responses; two-component Doppler global velocimeter; uniform jet flow; vapor-limited iodine cells; Aerospace engineering; Displays; Fluid flow measurement; Lenses; Light scattering; Particle scattering; Signal to noise ratio; Spatial resolution; Velocity measurement; Wire;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 2001. 19th International Congress on ICIASF 2001
  • Conference_Location
    Cleveland, OH
  • Print_ISBN
    0-7803-7022-8
  • Type

    conf

  • DOI
    10.1109/ICIASF.2001.960254
  • Filename
    960254