日本航空学会誌
Online ISSN : 2432-3039
Print ISSN : 0021-4663
極超音速プラズマ流におけるラングミュア・プ口ーブ測定
神元 五郎西田 迪雄
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ジャーナル フリー

14 巻 (1966) 144 号 p. 1-7

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Langmuir probe measurements have been performed in order to evaluate the properties of the flow in the working section of a plasma jet windtunnel. A single plane Langmuir probe has been used for conditions when the probe-collecting surface is parallel to the flow and the diameter of it is of the same order as the meam free path of a neutral atom. Electron temperature and Plasma density are calculated from Langmuir probe chharacteristics. A typical electrorn temperature is 3×103°K and a typical plasma density is 1013 particles/cm3.

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© The Japan Society for Aeronautical and Space Sciences
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