• DocumentCode
    2929359
  • Title

    Temperature Correction of PSP Measurement for Low-Speed Flow Using Infrared Camera

  • Author

    Mitsuo, Kazunori ; Kurita, Mitsuru ; Nakakita, Kazuyuki ; Watanabe, Shigeya

  • Author_Institution
    Wind Tunnel Technology Center, Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency, 7-44-1, Jindaijihigashi-Machi, Chofu-Shi, Tokyo, 182-8522, JAPAN. Email Address: mitsuo.kazunori@jaxa.jp
  • fYear
    2005
  • fDate
    2005
  • Firstpage
    214
  • Lastpage
    220
  • Abstract
    Pressure-Sensitive Paint (PSP) system combined with an infrared (IR) camera has been developed at 2 m x 2 m low-speed wind tunnel at WINTEC/JAXA. The temperature correction of PSP was conducted using both temperature image acquired by the IR camera and wind-off images immediately after the wind tunnel shutdown. As a verification test, the pressure distribution on a supersonic transfer (SST) model was measured by the PSP/IR combined system. The measurement accuracy was fairly improved compared to the previous method, i.e., the temperature correction of PSP using only wind-off PSP images immediately after wind tunnel shutdown.
  • Keywords
    Aerospace testing; Cameras; Fluid flow measurement; Measurement techniques; Paints; Pressure measurement; Space technology; System testing; Temperature dependence; Temperature sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 2005. iciasf '05. 21st International Congress on
  • Print_ISBN
    0-7803-9096-2
  • Type

    conf

  • DOI
    10.1109/ICIASF.2005.1569925
  • Filename
    1569925