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Peculiarities of high-temperature two-phase flow of combustion products in channels with an intentionally structured system of shock-waves

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Thermophysics and Aeromechanics Aims and scope

Abstract

Theoretical and simulation study was carried out for eliciting conditions when an intentionally formed system of oblique shocks can be used for control of parameters of condensed phase in supersonic flow. The key features of flow were analysed for two versions of duct, which are different in geometry of nozzle and acceleration headpiece. The results confirmed the feasibility of intentional impact on the structure of developing set of shock waves through changes in the duct profile: this would change the particle trajectories.

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References

  1. Y.V. Polezhaev and D.S. Mikhatulin, Heat Transfer in Heterogeneous Flow, Machine Engineering, Encyclopedia, in 40 vols, Vols. 1–2, Theoretical Mechanics, Thermodynamics, Heat Transfer, Chapt. 5, Mashinostroenie, Moscow, 1999. P. 383–433.

    Google Scholar 

  2. R.G. Boothroyd, Flowing Gas-Solids Suspensions, Chapman and Hall, London, 1971.

    Google Scholar 

  3. Two-Phase Mono-and Polydisperse Gas Flow with Suspended Particles, L.E. Sternin (Ed.), Mashinostroenie, Moscow, 1980.

    Google Scholar 

  4. N.N. Yanenko, R.I. Soloukhin, A.N. Papyrin, and V.M. Fomin, Supersonic Two-Phase Flow under Condition of Velocity Inequilibrium of Suspended Particles, Nauka, Novosibirsk, 1980.

    Google Scholar 

  5. L.E. Sternin, Fundamental Gas Dynamics for Two-Phase Flow in Nozzle, Mashinostroenie, Moscow, 1974.

    Google Scholar 

  6. A.M. Sizov, Gas Dynamics and Heat Transfer in Gas Jets for Metallurgic Processes, Metallurgia, Moscow, 1987.

    Google Scholar 

  7. K. Hoffman and S. Chiang, Computational Fluid Dynamics, Fourth ed., Engineering Education System, Kansas, 2000, Vol. 1, p. 486; Vol. 2. P 469; Vol. 3, P. 175.

    Google Scholar 

  8. A. Pollard and R. Martinuzzi, Comparative study of turbulence models in predicting turbulent pipe flow. II — Reynolds stress and k-ɛ models, AIAA J., 1989, Vol. 27, No. 12, P. 1714–1721.

    MATH  Google Scholar 

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Authors and Affiliations

  1. Bauman Moscow State Technical University, Moscow, Russia

    A. V. Voronetsky, S. A. Suchkov & L. A. Filimonov

Authors
  1. A. V. Voronetsky
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  2. S. A. Suchkov
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  3. L. A. Filimonov
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Additional information

This research was financially supported by the Russian Foundation for Basic Research (Grant No. 05-08-01414-a).

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Voronetsky, A.V., Suchkov, S.A. & Filimonov, L.A. Peculiarities of high-temperature two-phase flow of combustion products in channels with an intentionally structured system of shock-waves. Thermophys. Aeromech. 14, 201–210 (2007). https://doi.org/10.1134/S0869864307020060

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  • DOI: https://doi.org/10.1134/S0869864307020060

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