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Numerical and Experimental Studies on Non Equilibrium Flows in MPD Arc Jets.

Research Project

Project/Area Number 07651128
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionTokai University

Principal Investigator

KIMURA Itsuro  Tokai Univ.Aero Space Eng.Professor, 工学部, 教授 (20010697)

Co-Investigator(Kenkyū-buntansha) HORISAWA Hideyuki  Tokai Univ.Precision Eng.Lecturer, 工学部, 講師 (30256169)
Project Period (FY) 1995 – 1996
Project Status Completed (Fiscal Year 1996)
Budget Amount *help
¥2,000,000 (Direct Cost: ¥2,000,000)
Fiscal Year 1996: ¥900,000 (Direct Cost: ¥900,000)
Fiscal Year 1995: ¥1,100,000 (Direct Cost: ¥1,100,000)
KeywordsArc Jet / MPD Arc Jet / Non-Equilibrium Flow / 数値シミュレーション / 分子分光分析 / 陽極形状 / コンストリクタ
Research Abstract

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.

Report

(3 results)
  • 1996 Annual Research Report   Final Research Report Summary
  • 1995 Annual Research Report
  • Research Products

    (14 results)

All Other

All Publications (14 results)

  • [Publications] 堀澤 秀之: "プラズマジェットにおけるコンストリクタサイズの最適化に関する研究" 日本機械学会第74期全国大会講演論文集(III). No.96-15. 365-366 (1996)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 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)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 宮岡 和城: "プラズマジェットにおけるコンストリクタサイズの最適化" 1997年度精密工学会春季大会学術講演会. (発表予定). (1997)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 堀澤 秀之: "Optimization of Arc Constrictor Size in Low Power Arcjet Thruster" 33^<rd> AIAA/ASME/SAE/ASEE Joint Propulsion Conference. (発表決定)97-3202. (1997)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 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)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 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)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] MIYAOKA Kazuki: "Optimum Size of Constrictors in Plasma Jets (in Japanese)" Spring Lecture Meeting of Jap.Precision Soc.(to be published). (1997)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] KATO Ryoichi: "Numerical Simulation of Flame-Stabilization and Combustion Promotion by Plasma Jets in Supersonic Air Streams." Proc.26th Int.Sympo.on Combustion. (in printing). (1996)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 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)

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      1996 Final Research Report Summary
  • [Publications] 堀澤秀之: "プラズマジェットにおけるコンストリクタサイズの最適化に関する研究" 日本機械学会第74期全国大会講演論文集(III). No.96-15. 365-366 (1996)

    • Related Report
      1996 Annual Research Report
  • [Publications] 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)

    • Related Report
      1996 Annual Research Report
  • [Publications] 宮岡和城: "プラズマジェットにおけるコンストリクタサイズの最適化" 1997年度精密工学会春季大会学術講演会. (発表予定). (1997)

    • Related Report
      1996 Annual Research Report
  • [Publications] 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)

    • Related Report
      1995 Annual Research Report
  • [Publications] 加藤亮一: "高速気流中におけるプラズマジェットによる着火・保炎の数値解析" 航空原動機・宇宙推進講演会講演集(日本航空宇宙学会). 36. 243-248 (1996)

    • Related Report
      1995 Annual Research Report

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Published: 1995-04-01   Modified: 2016-04-21  

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