In this study, a simple model was developed to describe the mechanism behind a nonintrusive method that uses air glow discharge to simultaneously measure the gas density and temperature in low-density, short-duration hypersonic facilities. The developed model revealed that the emission intensity of the second positive band system of nitrogen molecules varies linearly with the gas density, which was firmly supported by spectroscopic observations characterizing the glow spectra. A laminar separated boundary layer was visually distinguishable via variations in the emission color reflected on a uniform positive column, along which traverse measurements were performed using miniature spectrometers. The experimental spectra agreed fairly well with synthetic ones calculated by substituting gas temperature distribution determined from computational fluid dynamics. In contrast, the temperature was not found to be a crucial factor determining the emission color distribution. The color was instead found to vary with the ratio of the emission intensity of the first positive band system to that of the second one. The principle of the variation in emission color implies that the mechanism explaining the variation will be more complex than what is assumed in existing models.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Potential of Glow-Discharge Flow Measurement in Hypersonic Low-Density Flows


    Contributors:
    Itoh, H. (author) / Mizoguchi, M. (author)

    Published in:

    AIAA Journal ; 58 , 1 ; 291-303


    Publication date :

    2019-10-21


    Size :

    13 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Plasmadynamics of Glow Discharge in Hypersonic Internal Flows

    Surzhikov, Sergey / Shang, Joseph | AIAA | 2007



    Velocity Measurement in Hypersonic Flows Using Electron-Beam-Assisted Glow Discharge

    S. Larigaldie / D. Bize / A. K. Mohamed et al. | AIAA | 1998


    Plasmadynamics of Glow Discharge in Hypersonic Internal Flows AIAA Paper

    Surzhikov, S. / Shang, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007


    Glow Discharge Visualization of Hypersonic Separated Flow past Cylinder/Plate Juncture

    Itoh, Hajime / Ishida, Takahiro / Miyoshi, Yohei et al. | AIAA | 2014