• DocumentCode
    2068301
  • Title

    Development of Bi-Luminophore Pressure-Sensitive Paint Systems

  • Author

    Mitsuo, Kazunori ; Kurita, Mitsuru ; Nakakita, Kazuyuki ; Fujii, Keisuke ; Watanabe, Shigeya ; Katagiri, Shinya ; Wada, Yuji

  • Author_Institution
    Japan Aerosp. Exploration Agency, Tokyo
  • fYear
    2007
  • fDate
    10-14 June 2007
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    Bi-luminophore pressure-sensitive paint (bi-PSP) has been developed in order to correct the error due to temperature dependence of PSP and increase PSP measurement accuracy. The bi-PSP was composed of pressure-and temperature-sensitive dye. Tetranuclear europium (III) complexes and PdTFPP were used as temperature-and pressure-sensitive dye, respectively. The luminescence intensity of the Eu complex was highly sensitive to temperature and insensitive to pressure. The bi-PSP was examined using a painted coupon and its characteristics were clarified. As a verification test, pressure distributions on a supersonic transport (SST) model at low-speed flow were acquired by the bi-PSP measurement system. The root mean square of Cp at 50m/s was approximately 0.1 (150 Pa) at flow speed of 50m/s, indicating that this bi-PSP system can measure more accurately pressure than conventional pressure conversion technique using reference PSP images immediately after stop of wind tunnel free stream. Furthermore, pressure images at angles of side-slip were clearly visualized, although PSP/temperature-sensitive paint (TSP) combined system can not acquire the overall pressure images of the whole model surface.
  • Keywords
    aerodynamics; dyes; flow visualisation; luminescence; paints; pressure measurement; supersonic flow; wind tunnels; aerodynamics; bi-luminophore pressure-sensitive paint system; flow visualisation; luminescence intensity; pressure 150 Pa; pressure-sensitive dye; pressure-sensitive paint image; supersonic transport model; temperature-sensitive dye; tetranuclear europium (III) complexes; velocity 50 m/s; wind tunnel free stream; Error correction; Fluid flow measurement; Luminescence; Paints; Pressure measurement; Root mean square; System testing; Temperature dependence; Temperature sensors; Velocity measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 2007. ICIASF 2007. 22nd International Congress on
  • Conference_Location
    Pacific Grove, CA
  • Print_ISBN
    978-1-4244-1599-1
  • Electronic_ISBN
    978-1-4244-1600-4
  • Type

    conf

  • DOI
    10.1109/ICIASF.2007.4380885
  • Filename
    4380885