Numerical Modeling of plasma flow in an Electrohydrodynamic thruster with two-cathode electrode arrangement
corona discharge which had been considered undesired before, has become popular for different uses in the past decades; including space thrusters. The basic corona discharge has a simple setup including two electrodes with unequal cross-sections; one of which connected to a high voltage and the othe...
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| 主要な著者: | , |
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| フォーマット: | Artigo |
| 言語: | Persa |
| 出版事項: |
Aerospace Research Institute
2019-07-01
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| シリーズ: | فصلنامه علوم و فناوری فضایی |
| 主題: | |
| オンライン･アクセス: | https://jsst.ias.ir/article_82177_7c3ed465d828806e0450d4921c5d05b4.pdf |
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