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Aerodynamic Heating in Three-Dimensional Bow Shock Wave/Turbulent Boundary Layer Interaction Region

  • Syozo Maekawa
  • Shigeru Aso
  • Shigehide Nakao
  • Kazuo Arashi
  • Kenji Tomioka
  • Hiroyuki Yamao
Conference paper

Abstract

Aerodynamic heating phenomena in the shock wave/turbulent boundary layer interaction region are one of the most important research tasks and this subject demands further investigation. To explain these phenomena, we investigate the bow shock wave/turbulent boundary layer interaction region induced by a blunt body, that is to say, the model case of the internal flow between a main rocket body and an auxiliary rocket booster. In this study, selecting as the main parameter the distance from the flat plate to the blunt body, the effect of the height is investigated by use of oil flow technique, surface pressure measurements and surface heat flux measurements. The results show that the distance has a major impact on the interaction region. Moreover, this parameter influences the flow behaviour.

Key words

Aerodynamic heating Shock wave Turbulent boundary layer Interaction 

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References

  1. Aso S, Kuranaga S, Nakao S (1990) Aerodynamic heating phenomena in three-dimensional shock wave/turbulent boundary layer interactions induced by sweptback blunt fins. AIAA Paper 90–0381Google Scholar
  2. Dolling DS, Bogdonoff SM (1982) Blunt fin induced shock wave/turbulent boundary layer interaction. AIAA J. 20: pp.1674–1680CrossRefADSGoogle Scholar
  3. Kaufmann LG, Johnson CB (1974) Interference heating from interactions of shock waves with turbulent boundary layer at Mach 6. NASA TM D-7469Google Scholar
  4. Korkegi RH (1971) Survey of viscous interaction associated with high Mach number flight. AIAA J. 9, 5:771–784CrossRefADSGoogle Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 1995

Authors and Affiliations

  • Syozo Maekawa
    • 1
  • Shigeru Aso
    • 1
  • Shigehide Nakao
    • 1
  • Kazuo Arashi
    • 2
  • Kenji Tomioka
    • 3
  • Hiroyuki Yamao
    • 4
  1. 1.Department of Aeronautics and AstronauticsKyushu UniversityFukuoka 812Japan
  2. 2.Churyo Engineering, Co. Ltd.NagoyaJapan
  3. 3.NASDATokyoJapan
  4. 4.Mitsubishi Heavy IndustryNagoyaJapan

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