• DocumentCode
    1409807
  • Title

    Langmuir Probe and Microwave Technique for Ionized Flows

  • Author

    Lederman, Samuel ; Wilson, Daniel ; Dawson, Edward

  • Author_Institution
    Department of Aerospace Engineering, Polytechnic Institute of Brooklyn, Farmingdale, N. Y.
  • Issue
    2
  • fYear
    1967
  • fDate
    3/1/1967 12:00:00 AM
  • Firstpage
    327
  • Lastpage
    338
  • Abstract
    Electron number densities were measured behind the incident shock wave in a pressure-driven shock tube by a microwave resonant cavity technique and by electrostatic probes. The driven gas was air at initial pressures of 0.5 and 1 mm Hg, and the shock Mach number was varied from 7 to 10. Electron neutral collision frequency was also determined by the microwave technique. The experimental measurements were compared with other measurements and with theory.
  • Keywords
    Density measurement; Electric shock; Electron tubes; Electrostatic measurements; Mercury (metals); Microwave measurements; Microwave theory and techniques; Probes; Resonance; Shock waves; Electron density; Langmuir probe; hypersonic; ionized flow; microwave; shock tube;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1967.5408759
  • Filename
    5408759