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Supersonic Combustion Flow Visualization at Hypersonic Flow

  • T. V. C. Marcos
  • D. Romanelli Pinto
  • G. S. Moura
  • A. C. Oliveira
  • J. B. ChanesJr.
  • P. G. P. Toro
  • M. A. S. Minucci
Conference paper

Introduction

Currently, a new generation of scientific aerospace vehicles, using advanced hypersonic airbreathing propulsion based on supersonic combustion technology, is in development at several research centers [1].

Keywords

Mach Number Oblique Shock Hypersonic Flow Oblique Shock Wave Schlieren Photograph 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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    Curran, E.T.: Scramjet Engines: The First Forty Years. Journal of Propulsion and Power 17(6) (November-December 2001)Google Scholar
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    Rolim, T.C., Minucci, M.A.S., Toro, P.G.P., Soviero, P.A.O.: Experimental Results of a Mach 10 Conical-Flow Derived Waverider. In: 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, AIAA 2009-7433 (2009)Google Scholar
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    Wang, Y., Zhang, D., Deng, X.: Design of Waverider Configuration with High Lift-Drag Ratio. Journal of Aircraft 44(1), 144–148 (2007)MathSciNetCrossRefGoogle Scholar
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    Heiser, W.H., Pratt, D.T., Daley, D.H., Mehta, U.B.: Hypersonic Airbreathing Propulsion. AIAA Education Series, 594 p. AIAA (1994)Google Scholar
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    Nagamatsu, H.T.: Shock Tube Technology and Design. In: Ferri, A. (ed.) Fundamental Data Obtained from Shock Tube Experiments, ch. III. Pergamon Press (1961)Google Scholar
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    Nascimento, M.A.C.: Gaseous Piston Effect in Shock Tube/Tunnel When Operating in the Equilibrium Interface Condition. Doctoral Thesis. Instituto Tecnológico de Aeronáutica - ITA, São José dos Campos, SP, Brazil (October 1997) (in English)Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 2012

Authors and Affiliations

  • T. V. C. Marcos
    • 1
  • D. Romanelli Pinto
    • 1
  • G. S. Moura
    • 1
  • A. C. Oliveira
    • 1
  • J. B. ChanesJr.
    • 1
  • P. G. P. Toro
    • 1
  • M. A. S. Minucci
    • 1
  1. 1.Prof. Henry T. Nagamatsu Laboratory of Aerothermodynamics and HypersonicsInstitute for Advanced StudiesSão José dos CamposBrazil

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