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Parameters and characteristics of a thermogasdynamic homogeneous reactor of overheated kerosine in an oncoming supersonic flow

  • Combustion, Explosion, and Shock Waves
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Abstract

The parameters and characteristics of a gas-air nosecone consisting of a flow of superheated kerosene vapor and its free boundary layer were determined. The flow and its boundary layer are considered as homogeneous vortex reactor formed on cocurrent and perpendicular vapor jets. The perpendicular vapor jets are fed along a central-axial multisection retractable needle mounted at the aircraft nose. The angle of inclination and flow rates of the jets of onboard fuel increase progressively along the needle.

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References

  1. E. S. Shchetinkov, Physics of Gas Combustion (Nauka, Moscow, 1965) [in Russian].

    Google Scholar 

  2. E. S. Shetinkov, Astronaut. Acta 15, 597 (1970).

    Google Scholar 

  3. E. S. Shchetinkov, Combustion in Turbulent Flow (Akad. Nauk SSSR, Moscow, 1959) [in Russian].

    Google Scholar 

  4. M. R. Koliev, A. G. Prudnikov, V. V. Severinova, et al., in Proc. 7th Intern. School-Seminar on Models and Methods of Aerodynamics (MTsNMO, Moscow, 2007), p. 172.

    Google Scholar 

  5. Yu. N. Nechaev, A. G. Prudnikov, and A. G. Roshchin, Polet, No. 1, 10 (2004).

  6. Yu. N. Nechaev, A. G. Prudnikov, N. N. Zakharov, et al., in Proc. 31st Acad. Readings on Cosmonautics in Honour of 100 Years of Acad. S.P. Korolev’s Birthday (IIET, Moscow, 2007), p. 369.

    Google Scholar 

  7. A. G. Prudnikov, N. N. Zakharov, V. K. Verkholomov, et al., in TsIAM 2001–2005, Main Results of Sci.-Tech. Activity, Annivers. Collection to 75 Years of TsIAM Baranova (TsIAM, Moscow, 2005), Vol. 1, p. 370 [in Russian].

    Google Scholar 

  8. A. G. Prudnikov, Dvigatel’, No. 2, 18 (2007).

  9. A. Rochko, AIAA J. 14, 1349 (1976).

    Article  Google Scholar 

  10. A. G. Prudnikov, in Works of TsIAM (TsIAM, Moscow, 1987), No. 1191, p. 40 [in Russian].

    Google Scholar 

  11. A. I. Zubkov, A. G. Prudnikov, and P. K. Tret’yakov, in Proc. of the 8th Intern. School-Seminar on Models and Methods of Aerodynamics (Evpatoria, 2008), p. 26.

  12. A. G. Prudnikov, M. R. Koliev, V. V. Severinova, and P. K. Tret’yakov, Aviakosm. Tekhn. Tekhnol., No. 3, 10 (2007).

  13. G. N. Abramovich, Applied Gas Dynamics (Nauka, Moscow, 1969) [in Russian].

    Google Scholar 

  14. A. V. Prudnikov, Aviakosm. Tekhn. Tekhnol., No. 1, 11 (2008).

  15. A. G. Prudnikov, M. S. Volynskii, and V. N. Sagalovich, Processes of Mixing and Combustion in Jet Engines (Mashinostroenie, Moscow, 1971) [in Russian].

    Google Scholar 

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Authors and Affiliations

  1. Baranov Central Institute of Aviation Motors Development, Moscow, Russia

    A. G. Prudnikov

  2. Semenov Institute of Chemical Physics, Russian Academy of Sciences, Moscow, Russia

    A. V. Roshchin

  3. Moscow Aviation Institute (State University of Aerospace Technologies), Moscow, Russia

    E. O. Pozdeeva

  4. Skobel’tsin Institute of Nuclear Physics, Moscow State University, Moscow, Russia

    E. O. Pozdeeva

Authors
  1. A. G. Prudnikov
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  2. A. V. Roshchin
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  3. E. O. Pozdeeva
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Corresponding author

Correspondence to A. V. Roshchin.

Additional information

Original Russian Text © A.G. Prudnikov, A.V. Roshchin, E.O. Pozdeeva, 2010, published in Khimicheskaya Fizika, 2010, Vol. 29, No. 12, pp. 32–39.

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Prudnikov, A.G., Roshchin, A.V. & Pozdeeva, E.O. Parameters and characteristics of a thermogasdynamic homogeneous reactor of overheated kerosine in an oncoming supersonic flow. Russ. J. Phys. Chem. B 4, 977–984 (2010). https://doi.org/10.1134/S1990793110060163

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  • DOI: https://doi.org/10.1134/S1990793110060163

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