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Gas Heating Effects in a Nanosecond-Pulse Streamer Discharge Interacting With a Supersonic \hbox {O}_{2}{-}\hbox {H}_{2} Flow

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2 Author(s)
Breden, D. ; Dept. of Aerosp. Eng. & Eng. Mech., Univ. of Texas at Austin, Austin, TX, USA ; Raja, L.L.

We discuss gas heating effects in an anodic-pulse 4-kV 10-ns discharge interacting with a Mach 3 supersonic premixed O2-H2 boundary layer flow. Rapid gas heating occurs in the electrode near-field region with gas temperature increase on the order of 100 K-200 K. The rapid heating of the gas mixture results in micro blast waves which propagate into the free stream and eventually decay.

Published in:

Plasma Science, IEEE Transactions on  (Volume:39 ,  Issue: 11 )