46th AIAA Aerospace Sciences Meeting and Exhibit 2008
DOI: 10.2514/6.2008-1104
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Experimental Study of a Fast Ionization Wave Discharge at High Pulse Repetition Rates

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Cited by 7 publications
(2 citation statements)
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“…In this case, the positive polarity terminal of the pulser (+16 kV) was connected to the 'high voltage electrode', and the negative polarity terminal (−16 kV) was connected to the 'grounded electrode' and the waveguide outside the cell (see figure 1(a)). This 'dual polarity' ionization wave generated by this pulser, similar to the one used in our previous work [10], was used to reduce significantly pulse voltage rise time and increase peak voltage difference between the electrodes. Note that the voltage between the electrodes may be higher than the difference between the incident pulse peak voltages (by up to a factor of two), due to incident voltage pulse reflection.…”
Section: Methodsmentioning
confidence: 99%
“…In this case, the positive polarity terminal of the pulser (+16 kV) was connected to the 'high voltage electrode', and the negative polarity terminal (−16 kV) was connected to the 'grounded electrode' and the waveguide outside the cell (see figure 1(a)). This 'dual polarity' ionization wave generated by this pulser, similar to the one used in our previous work [10], was used to reduce significantly pulse voltage rise time and increase peak voltage difference between the electrodes. Note that the voltage between the electrodes may be higher than the difference between the incident pulse peak voltages (by up to a factor of two), due to incident voltage pulse reflection.…”
Section: Methodsmentioning
confidence: 99%
“…Recent advances in nanosecond pulse discharge plasma [15][16][17][18][19] and direct driving of short pulse width [20,21] are expected to permit uniform discharge in supersonic air flow. This paper established an experimental system for nanosecond pulse discharge under supersonic conditions, and investigated discharge and displacement current characteristics under static condition and air flow velocity at Mach 2.…”
Section: Introductionmentioning
confidence: 99%