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Unified Numerical Analysis of Galileo Probe Entry Flight Flowfield with Radiation and Ablation

Research Project

Project/Area Number 15560129
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Fluid engineering
Research InstitutionTohoku University

Principal Investigator

SAWADA Keisuke  Tohoku University, Graduate School of Engineering, Professor, 大学院・工学研究科, 教授 (80226068)

Project Period (FY) 2003 – 2005
Project Status Completed (Fiscal Year 2005)
Budget Amount *help
¥3,500,000 (Direct Cost: ¥3,500,000)
Fiscal Year 2005: ¥900,000 (Direct Cost: ¥900,000)
Fiscal Year 2004: ¥900,000 (Direct Cost: ¥900,000)
Fiscal Year 2003: ¥1,700,000 (Direct Cost: ¥1,700,000)
Keywordsablation / radiation / Galileo probe vehicle / hydrogen / multiband radiation model / recession / turbulent transition / tightly coupled calculation / ガリレオ探査衛星 / マルハバンド輻射モデル
Research Abstract

In 1995, the Galileo probe vehicle launched by NASA entered into the Jovian atmosphere at a velocity of 49 km/s. The probe vehicle was thermally protected by ablative heatshield. According to the actual flight data, the amount of heatshield recession at the stagnation point was found to be halved and that at the frustum region was doubled than those given by the preflight prediction.
In this study, the strongly radiating flowfield over the Galileo probe vehicle is numerically obtained using the newly developed computer code, in which we assume the thermochemical equilibrium flowfield and also the steady ablation of the heatshield. For the first time, we have successfully reproduced the amount of heatshield recession at the frustum region. We have also identified the cause of enhanced radiative heating occurred at the frustum region. It is however indicated that the amount of heatshield recession at the stagnation region is still overestimated. This is probably caused by nonequilibrium effect in the shock layer that is not accounted for in this study. Although the nonequilibrium effect itself reduces the amount of radiative heating at the stagnation region, a more accurate prediction method is certainly needed to reduce the weight of heatshield and maximize payload in the design of future probe vehicles.
As a preliminary step, we have optimized the multiband radiation model for the mixture of hydrogen and helium. At higher temperatures, the radiative property of atomic hydrogen is critically influenced by the number density of electron. Therefore, the newly developed multiband model accounts not only for the translational temperature of the gas but also for the number density of electron, simultaneously. The accuracy of the model is critically assessed. The developed radiation model will be employed in the computer simulation of nonequilibrium ionization of hydrogen observed in various shock tube experiments.

Report

(4 results)
  • 2005 Annual Research Report   Final Research Report Summary
  • 2004 Annual Research Report
  • 2003 Annual Research Report
  • Research Products

    (16 results)

All 2006 2005 2004 2003 Other

All Journal Article (13 results) Publications (3 results)

  • [Journal Article] Multiband Radiation Model for Simulation of Galileo Probe Entry Flowfield2006

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Journal of Thermophysics and Heat Transfer (to appear)

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Multiband Radiation Model for Simulation of Galileo Probe Entry Flowfield2006

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Journal of Thermophysics and Heat Transfer (in press)

    • Related Report
      2005 Annual Research Report
  • [Journal Article] Numerical Simulation of Galileo Probe Entry Flowfield with Radiation and Ablation2005

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Journal of Thermophysics and Heat Transfer 19・1

      Pages: 28-35

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2005 Annual Research Report 2005 Final Research Report Summary 2004 Annual Research Report
  • [Journal Article] Experimental and Numerical Study of Pyrolysis Gas Pressure in Ablating Test Piece2005

    • Author(s)
      Toshiyuki Suzuki
    • Journal Title

      Journal of Thermophysics and Heat Transfer 19・3

      Pages: 266-272

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Numerical Simulation of Galileo Probe Entry Flowfield with Radiation and Ablation2005

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Journal of Thermophysics and Heat Transfer Vol.19, No.1

      Pages: 28-35

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Experimental and Numerical Study of Pyrolysis Gas Pressure in Ablating Test Piece2005

    • Author(s)
      Toshiyuki Suzuki
    • Journal Title

      Journal of Thermophysics and Heat Transfer Vol.19, No.3

      Pages: 266-272

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Experimental and Numerical Study of Pyrolysis Gas Pressure in Ablating Test Piece2005

    • Author(s)
      Tohshiyuki Suzuki
    • Journal Title

      Journal of Thermophysics and Heat Transfer 19・3

      Pages: 266-272

    • Related Report
      2005 Annual Research Report
  • [Journal Article] Gas Permeability of Oblique-Layered Carbon-Cloth Ablator2004

    • Author(s)
      Toshiyuki Suzuki
    • Journal Title

      Journal of Thermophysics and Heat Transfer 18・4

      Pages: 548-550

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Gas Permeability of Oblique-Layered Carbon-Cloth Ablator2004

    • Author(s)
      Toshiyuki Suzuki
    • Journal Title

      Journal of Thermophysics and Heat Transfer Vol.18, No.4

      Pages: 548-550

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Parallel Computation of Fully-Coupled Hypersonic Radiating Flowfield Using Multi-Band Model2003

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Journal of Thermophysics and Heat Transfer 17・1

      Pages: 21-28

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Distributed-Memory Parallelization of Radiative Transfer Calculation in Hypersonic Flow2003

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Parallel Computational Fluid Dynamics --- New Frontiers and Multi-Disciplinary Applications(Eds. K. Matsuno, A. Ecer, J. Periaux, N. Satofuka, P. Fox)

      Pages: 491-498

    • Description
      「研究成果報告書概要(和文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Parallel Computation of Fully-Coupled Hypersonic Radiating Flowfield Using Multi-Band Model2003

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Journal of Thermophysics and Heat Transfer Vol.17, No.1

      Pages: 21-28

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Journal Article] Distributed-Memory Parallelization of Radiative Transfer Calculation in Hypersonic Flow2003

    • Author(s)
      Shingo Matsuyama
    • Journal Title

      Parallel Computational Fluid Dynamics --- New Frontiers and Multi-Disciplinary Applications(Eds.K.Matsuno, A.Ecer, J.Periaux, N.Satofuka, and P.Fox)

      Pages: 491-498

    • Description
      「研究成果報告書概要(欧文)」より
    • Related Report
      2005 Final Research Report Summary
  • [Publications] Shinogo Matsuyama: "Parallel Computation of Fully-Coupled Hypersonic Radiating Flowfield Using Multi-Band Model"Journal of Thermophysics and Heat Transfer. 17・1. 21-28 (2003)

    • Related Report
      2003 Annual Research Report
  • [Publications] Shinogo Matsuyama: "Distributed-Memory Parallelization of Radiative Transfer Calculation in Hypersonic Flow"Parallel Computational Fluid Dynamics -- New Frontiers and Multi-Disciplinary Applications. 491-498 (2003)

    • Related Report
      2003 Annual Research Report
  • [Publications] Shinogo Matsuyama: "Trajectory-Based Heating Analysis of Galileo Probe Entry Flowfield with Radiation and Ablation"AIAA Paper 2003-3768. 1-10 (2003)

    • Related Report
      2003 Annual Research Report

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Published: 2003-04-01   Modified: 2016-04-21  

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