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1995 Fiscal Year Final Research Report Summary

EFFECT OF NONEQUILIBRIUM BEHIND A STRONG SHOCK UPON RE-ENTRY AERODYNAMIC HEATING

Research Project

Project/Area Number 05452305
Research Category

Grant-in-Aid for General Scientific Research (B)

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionKYUSHU UNIVERSITY

Principal Investigator

NISHIDA Michio  KYUSHU UNIV., DEPT.AERONAUTICS & ASTRONAUTICS,PROFESSOR, 工学部, 教授 (10025968)

Co-Investigator(Kenkyū-buntansha) KIHARA Hisashi  KYUSHU UNIV., DEPT.AERONAUTICS & ASTRONAUTICS,RESEARCH ASSOCIATE, 工学部, 助手 (60243911)
ASO Shigeru  KYUSHU UNIV., DEPT.AERONAUTICS & ASTRONAUTICS,ASSOCIATE PROFESSOR, 工学部, 助教授 (40150495)
Project Period (FY) 1993 – 1995
KeywordsRE-ENTRY AERODYNAMICS / RE-ENTRY AERODYNAMIC HEATING / NONEQUILIBRIUM FLOW / STRONG SHOCK WAVE / HYPERSONIC FLOWS / HIGH TEMPERATURE GAS / NUMERICAL STUDY / SPACE
Research Abstract

The atmospheric entry of space transportation systems at high altitudes generates a very strong shock wave. Such a shock wave causes vibrational excitation, dissociation and ionization of the shock layr gas, and the flow will be in thermal and chemical nonequilibrium due to very low density. Although rotational temperature is quickly equilibrated with translational temperature of heavy particle, vibrational temperature and electron temperature deviate from translational temperature. Therefore, in order to estimate re-entry aerodynamic heating, the following items should be revealed :
(1) Effect of thermal nonequilibrium : energy transfer rates among translational, vibrational and electron-translational energy modes,
(2) Radiative effect : Radiative intensity in high temperature gas behind a strong shock,
(3) Effects of wall conditions : effect of catalytic wall on aerodynamic heating, wall condition for vibrational temperature.
In the present investigations, nonequilibrium flows including the above three conditions are studied experimentally and numerically. In the numerical study of viscous shock layr (VSL) analysis of the thermochemical nonequilibrium flows over a blunt body, a three temperature model was treated and thereby the structure of nonequilibrium shock layr flows was revealed. In addition, the effect of wall catalysis on aerodynamic heating was investigated. Also, experiments were carried out using a piston-driven shock tube, and radiation spectrum emitting from the high-temperature gas behind a strong shock wave was observed. wall vibrational-condition has been deduced from theoretical analysis considering vibrational energy flux at the edge of Knudsen layr.

  • Research Products

    (17 results)

All Other

All Publications (17 results)

  • [Publications] 西田迪雄: "大型反射衝撃風洞とその計測技術" 日本航空宇宙学会誌. 42. 135-140 (1994)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] 西田迪雄: "衝撃波によって誘起される非定常ノズル流の数値計算" 日本機械学会論文集(B編). 60. 2267-2272 (1994)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Nonequilibrium Viscous Shock Layer Analysis Using a Three Temperature Model" Rarefied Gas Dynamics,Progress in Astro.and Aero.158. 401-412 (1994)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Rarefied Gas Flow over a Catalytic Wall" Rarefied Gas Dynamics,Progress in Astro.and Aero.159. 640-652 (1994)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Viscous Shock Layer Analysis Using a Three Temperature Model" Shock Waves (Springer Verlag). Vol II. 333-338 (1995)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Propagation Behavior of Strong Shock Waves with Chemical Reactions in a Shock Tunnel Nozzle" Shock Waves (Springer Verlag). Vol.II. 301-306 (1995)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Wall Slip Condition of Vibrational Temperature" Rarefied Gas Dynamis (Oxford Univ.Press). 981-987 (1995)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Viscous Shock Layer Analysis of Hypersonic Thermochemical Nonequilibrium Flows around the OREX Using a Three Temperature Model" Transactions of Japan Society of Heat and Fluid Engineering. 8. 1-11 (1995)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida: "Computation of Thermochemical Nonequilibrium Flows Using a Diagonal LU Implicit Scheme" JSME International. 38. 458-464 (1995)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] M.Nishida and Y.Sakamura: "Nonequilibrium Viscous Shock Layr Analysis Using a Three Temperature Model" Rarefied Gas Dynamics, Progress in Astronautics and Aeronautics. Vol.158. 401-412 (1994)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] K.Yamamoto, T.Nishitani and M.Nishida: "Rarefied Gas Flow over a Catalytic Wall" Rarefied Gas Dynamics, Progress in Astronautics and Aeronautics. Vol.159. 640-652 (1994)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] M.Nishida and Y.Sakamura: "Nonequilibrium Flows around a Hypersonic Reentry Vehicle Model" Proceedings of the Asian-Pacific Conference on Aerospace Technlogy and Science, International Academic Publishers, Beijing. 637-642 (1994)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] Y.Sakamura and M.Nishida: "Viscous Shock Layr Analysis Using a Three-Temperature Model" Shock Waves (R.Brun & L.Z.Dumitrescu, ed., Springer Verlag). Vol.II. 333-338 (1995)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] M.Nishida, K.Tanabe, Y.Sakamura and Y.Yamamoto: "Wall Slip Condition of Vibrational Temperature" Rarefied Gas Dynamics 19 (J.Harvey & G.Lord, ed., Oxford University Press). 981-987 (1995)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] Y.Sakamura, M.Nishida and T.Suzuki: "Viscous Shock Layr Analysis of Hypersonic Thermochemical Nonequilibrium Flows around the OREX Using a Three-Temperature Model" Transaction of Japan Society of Heat and Fluid Engineering. Vol.8, (July). 1-11 (1995)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] Y.Sakamura and M.Nishida: "Computation of Thermochemical Nonequilibrium Flows Using a Diagonal LU Implicit Scheme" JSME International. Vil.38, No.3 (August). 458-464 (1995)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] H.Okamoto, M.Nishida, T.Tanaka and A.Beylich: "Numerical Studies of an Arc-Heated Nozzle Flow for a Low Power Arcjet Thruster" Computational Fluid Dynamics JOURNAL. Vol.4, No.2, (July). 177-190 (1995)

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Published: 1997-03-04  

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