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
Link To Document :
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