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1997 Fiscal Year Final Research Report Summary

Investigation of Radiation-cooled Arc Heater

Research Project

Project/Area Number 07555607
Research Category

Grant-in-Aid for Scientific Research (A)

Allocation TypeSingle-year Grants
Section展開研究
Research Field Aerospace engineering
Research InstitutionKyushu University

Principal Investigator

NISHIDA Michio  Dept.of Aeronautics & Astronautics, Kyushu Univ.Professor, 工学部, 教授 (10025968)

Co-Investigator(Kenkyū-buntansha) MATSUMOTO Masashi  Research Institute, Ishikawajima-Harima Heavy Industries Co.Ltd.Research Enginee, 技術研究所, 研究員
KIHARA Hisashi  Dept.of Aeronautics & Astronautics, Kyushu Univ.Assistant, 工学部, 助手 (60243911)
ASO Shigeru  Dept.of Aeronautics & Astronautics, Kyushu Univ.Associate Prof., 工学部, 助教授 (40150495)
Project Period (FY) 1995 – 1997
KeywordsArc Heater / High Temperature Gas Dynamics / Arc-heated Wind Tunnel / Ionized Gas
Research Abstract

During atmospheric entry, a maximun flight Mach number is over 25 and a very strong shock wave is generated ahead of a nose and wings. Air temperature behind such a strong shock wave becomes over 10,000K and as a result nitrogen and oxygen molecules dissociated and ionized. In addition Nitric oxide is also produced due to the combination of dissociated molecules. An arc-heated wind tunnel can be considered as one of ground test facilities to similate the atmospheric entry conditions, that is to say, a high speed flow of dissociated and ionized air. A conventional arc heater is water-cooled but this water cooling system is considerable complex and sometimes an accident of water occurs. Therfore, in the present study, a radiation-cooled arc heated is proposed instead of a water-cooled arc heater. It is the present aim to develop such a radiation-cooled arc heater and to apply it to studies of high-enthalpy flows needed for the reeentry aerodynamic heating experiments
The following items have been done in 1997 :
(1) perforamnce test of a arc-heated wind tunnel
・arc current-arc voltage characteristics
・test gas flow rate-arc current characteristics
・arc current-stagnation enthalpy characteristics
(2) thermal characterics test
・stagnation heat flux measurements
・estimation of stagnation enthalpy
・estimation of heating efficiency

  • Research Products

    (7 results)

All Other

All Publications (7 results)

  • [Publications] M.Nishida M.Matsumoto: "Thermochemical Nonequilibrium in Rapidly Expannding Flows of High Temperature Air" Zeitschrift fuer Naturforschung. Vol.52a. 358-368 (1997)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida M.Matsumoto: "Numerical Analysis of Nonequilibrium Freejets Using a Multi Vibrational-Temperature Model" Rarefied Gas Dynamics 20(Peking University Press,Beijing). 531-536 (1997)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Hirakawa, S.Aso, M.Nishida, M.Matsumoto: "Arc-Heated Wind Tunnel Experiments" Proc.2nd Asian-Pacific Conf.on Aerospace Technology. 125-130 (1997)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] 西田 迪雄、他87名(分担執筆): "流体実験ハンドブック" 朝倉書店, 709 (1997)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida & M.Matumoto: "Thermochemical Nonequilibrium in Rapidly Expanding Flows of High Temperatuer Air" Zeitshrift fuer Naturforschung. Vol.52a. 358-368 (1997)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] M.Nishida & M.Matumoto: "Numerical Analysis of Nonequilibrium Freejets Using a Multi Vibratioanl Temperture Model" Rarefied Gas Dynamics 20 (Peking Univ.Press). 531-536 (1997)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] M.Hirakawa, S.Aso, M.Nishida & M.Matumoto: "Arc-Heated Wind Tunnel Experiments" Proc.2nd Asian-Pacific Conf.on Aerospace Technology & Science. 125-130 (1997)

    • Description
      「研究成果報告書概要(欧文)」より

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Published: 1999-03-16  

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