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2001 Fiscal Year Final Research Report Summary

Nonequilibrium Aerodynamics for a Super-orbital Reentry

Research Project

Project/Area Number 11694165
Research Category

Grant-in-Aid for Scientific Research (B)

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

Principal Investigator

NISHIDA Michio  Kyushu University, Dept Aeronautics & Astronautics, Professor, 工学研究院, 教授 (10025968)

Co-Investigator(Kenkyū-buntansha) SUZUKI Koujiro  University of Tokyo, Department of Advanced Energy, Associate Professor, 大学院・新領域創成科学研究科, 助教授 (10226508)
ABE Ken-ichi  Kyushu University, Dept Aeronautics & Astronautics, Associate Professor, 工学研究院, 助教授 (20315104)
ABE Takashi  Institute of Space and Astronautical Science, Professor, 宇宙輸送研究系, 教授 (60114849)
Project Period (FY) 1999 – 2001
KeywordsReentry / Hypersonic flows / Space transpotation / Nonequilibrium flows / Aerodynamic heating / Wall catalysis / Shock wave / Super-orbital reentry / アブレーション
Research Abstract

1. Investiation of a noneguilibrium shock layer around a super-orbital reentry capsule
Using the VSL (Viscous Shock Layer) method, a thermochemical nonequilibrium shock layer around a super-orbital orbital reentry space vehicle was numerically investigated. Heat flux on the vehicle wall was estimated from the computed flow properties. In addition, radiative heat flux was also calculated. It was revealed that the dominant spectra were the line spactra of N, O and N+ in the ultra-violet and vacuum ultra-violet region.
2. Ablation cooling
The VSL analysis was extended to a nonequilibrium shock layer with ablation cooling. The vehicle wall temperature for which the ablation cooling warks efficiently was investigated. The spectrum caused by the ablation was C swan band.
3. Structure of a very strong shock wave caused by a super-orbital reentry
A very strong shock wave was generated by a piston^driven shock tube and electron density was measured behind it using a one-dimensional imaging spectroscopic method developed by one of the invesigators of this research. The results showed that ionization rate was faster than that predicted by the conventional model.

  • Research Products

    (12 results)

All Other

All Publications (12 results)

  • [Publications] R.Doihara, M.Nishida: "The VSL Analysis of the Flow Field over a Super Orbital Reentry Capsule"Transactions of the Japan Society for Aeronautics and Space Science. Vol.44No.144. 73-81 (2001)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] R.Doihara, M.Nishida: "A Thermochemical Nonequilibrium Flow around a Super Orbital Reentry Capsule"Rarefied Gad Dynamics (22nd International Symposium, Sydney, Australia) (American Institute of Physics). 715-722 (2001)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] K.Fujita, A.Matsuda, S.Sato, T.Abe: "Precursor Electron Density Measurement ahead of Strong Shock Waves"Rarefied Gad Dynamics (22nd International Symposium, Sydney, Australia) (American Institute of Physics). 780-786 (2001)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] K.Fujita, S.Sato, T.Abe, A.Matsuda: "Electron Temperature and Density Measurement ahead of Strong Shod Waves"AIAA 2001-2765, 35th AIAA Thermophysics Conference. (2001)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] H.Otsu, N.Kanai, K.Fujita, T.Abe: "Effect of Models for Transport Properties on the Hypersonic Reentry Heating Environment"AIAA 2001-2831, 35th AIAA Thermophysics Conference. (2001)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] K.Suzuki, K.Koshino, K.Fukuta: "Numerical and Experimental Studies on Aerodynamic Heating Augmentation Induced by Gaps on Surface of Hypersonic Vehicle"Proc. 1st Taiwan-Japan Workshop on Mech. and Aerospace Eng.. 451-460 (2001)

    • Description
      「研究成果報告書概要(和文)」より
  • [Publications] R. Doihara, M. Nishida: "The VSL Analysis of the Flow Field over a Super Orbital Reentry Capsule"Transactions of the Japan Society for Aeronautics and Space Science. Vol. 44. 73-81 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] R. Doihara, M. Nishida: "A Thermochemical Nonequilibrium Flow around a Super Orbital Reentry Capsule"Rarefied Gad Dynamics (22nd International Symposium, Sydney, Australia) (American Institute of Physics). 715-722 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] K. Fujita, A. Matsuda, S. Sato, T. Abe: "Precursor Electron Density Measurement ahead of Strong Shock Waves"Rarefied Gad Dynamics (22nd International Symposium, Sydney, Australia) (American Institute of Physics). 780-786 (2001)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] K. Fujita, S. Sato, T. Abe, A. Matsuda: "Electron Temperature and Density Measurement ahead of Strong Shock Waves"AIAA 2001-2765, 35th AIAA Thermophysics Conference. (2001)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] H. Otsu, N. Kanai, K. Fujita, T. Abe: "Effect of Models for Transport Properties on the Hypersonic Reentry Heating Environment"AIAA 2001-2831, 35th AIAA Thermophysics Conference. (2001)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] K. Suzuki, K. Koshino, K. Fukuta: "Numerical and Experimental Studies on Aerodynamic Heating Augmentation Induced by Gaps on Surface of Hypersonic Vehicle"Proc. 1st Taiwan-Japan Workshop on Mech. and Aerospace Eng.. 451-460 (2001)

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

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Published: 2003-09-17  

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