• DocumentCode
    2834348
  • Title

    The use of pressure sensitive paints on rotating machinery

  • Author

    Burns, Steven P. ; Sullivan, John P.

  • Author_Institution
    Sch. of Aeronaut. & Astronaut., Purdue Univ., West Lafayette, IN, USA
  • fYear
    1995
  • fDate
    18-21 Jul 1995
  • Lastpage
    3214
  • Abstract
    The current work involves measuring the surface pressure on a rotating blade with a laser scanning pressure paint system. The pressure paint consists of a fluorescent molecule which is mixed with a binder than painted on the surface of interest. The laser is scanned across the model surface which excites the fluorescent molecule. The intensity with which the molecule emits light is dependent on the amount of oxygen quenching and therefore the local air pressure. The system can be calibrated in two ways. The first would be to take an intensity reading with the known pressure and then take a reading at the condition of interest. The Stern-Volmer relationship of intensities is used to calculate the pressure. A second way is to measure the decay time of the emitted intensity and calibrate that versus pressure. The purpose of the experiment is to get a complete surface map of the pressure on the rotating blade
  • Keywords
    aircraft testing; calibration; gas turbines; pressure measurement; wind tunnels; Stern-Volmer relationship; calibration; decay time; fluorescent molecule; intensity reading; laser scanning pressure paint system; oxygen quenching; pressure sensitive paints; rotating blade; surface map; surface pressure; Blades; Current measurement; Fluorescence; Laser excitation; Laser modes; Machinery; Paints; Pressure measurement; Rotation measurement; Surface emitting lasers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1995. ICIASF '95 Record., International Congress on
  • Conference_Location
    Wright-Patterson AFB, OH
  • Print_ISBN
    0-7803-2088-3
  • Type

    conf

  • DOI
    10.1109/ICIASF.1995.519463
  • Filename
    519463