Numerical and Experimental Studies on Non Equilibrium Flows in MPD Arc Jets.
Numerical and Experimental Studies on Non Equilibrium Flows in MPD Arc Jets.
批准号:
07651128
负责人:
KIMURA Itsuro
金额:
$1.28万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
1995
资助国家:
日本
项目状态:
已结题
起止时间:
1995 至 1996
中文摘要
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英文摘要
Numerical Studies on steady one-dimensional self-field MPD arc jets were conducted, taking into consideration the non-equilibrium ionization and dissociatin, and the thermal non-equilibrium. Following results were obtained :1. The current concentration is observed at the entrance and the exit of the channel in the case of argon and it is observed only at the exit of the channel in the case of hydrogen.2. The electrical conductivity is proportional to the 3/2 powers of electron temperature in the case of argon, while it is proportional to the root of that in the case of hydrogen.3. The operation of arc jets is influenced mainly by a characteristic velocity and entrance mach numbers, and also by a characteristic energy.Experimental studies on the effect of constrictor size and anode geometry (nozzle type, flare type, straight type) on the performance of arc jets were conducted using nitrogen or argon propellants. Following results were obtained :1. The electron temperature, the vibrational and rotational temperatures of molecules can be assumed in equilibrium in arc jets for the case of nitrogen propellant.2. The performance of arc jets is improved as the length and diameter of the constrictor are decreased, but the arc does not established under a critical diameter.3. The temperature and heat content of the gas ejected from arc jets are influenced by constrictor geometry but the effect of gas pressure on them is small.4. In the case of argon propellant, in the range of arc current, 50-350 A,the best performance was obtained for the flare type andhe with small diameter, operated at a low mass flow rate.
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堀澤 秀之: "プラズマジェットにおけるアーク・コンストリクタ・サイズに関する研究" 日本機械学会第74期通常総会講演会講演論文集(III). (発表予定). (1997)
Hideyuki Horisawa:“等离子射流中电弧收缩器尺寸的研究”日本机械工程师学会第 74 届普通大会论文集(III)(待提交)。
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堀沢秀之: "低電力プラズマジェットの開発および性能評価に関する研究" 日本機械学会全国大会講演論文集(III). 95. 274-275 (1995)
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HORISAWA Hideyuki: "Arc Constrictor Size in Plasma Jets. (in Japanese)" Proc.of Lectures in Gen.Meeting (74th) of Jap. Mech.Soc.(to be published). (1997)
堀泽秀幸:“等离子射流中的弧缩器尺寸。(日语)”日本 Gen.Meeting(第 74 届)讲座记录。
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OGIWARA Kazuhiko: "Study on 300W-Class Direct Current Arcjet Thruster." Proc.20th Int.Sympo.On Space Tech.and Sci.96-a-3-01. 1-8 (1996)
OGIWARA Kazuhiko:“300W级直流电弧喷射推进器的研究”。
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HORISAWA Hideyuki: "Optimum Size of Constrictors in Plasma Jets. (in Japanese)" Proc.74th Lecture Meeting of Jap.Mech.Soc.No.96-15. 365-366 (1996)
堀泽秀幸:“等离子射流中收缩器的最佳尺寸。(日语)”日本机械学会第 74 次演讲会第 96-15 号论文集。
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