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Characteristic features of diagnostics of supersonic high-temperature jet parameters

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Journal of Engineering Physics and Thermophysics Aims and scope

The distribution of the gas temperature over the radius of a supersonic high-temperature free underexpanded jet at different distances from the plasmatron nozzle cut, as well as the distribution of the stagnation pressure, heat flux, and shock layer thickness along the length of a supersonic high-temperature blocked jet, is investigated experimentally depending on the sensor diameter. It is shown that in the calculation of the Mach number, static pressure, and thermodynamic enthalpy of the air of the underexpanded jet (near the nozzle cut), it is necessary to account for the thickness of the shock layer formed upstream of the sensor.

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References

  1. V. V. Chuprasov, M. S. Tret’yak, and A. F. Klishin, Experimental rig for investigating the interaction of plasma jets with a substance, in: Abstracts of the Int. Conf. “Materials and Coatings under Extreme Conditions: Investigations, Application, Ecologically Pure Technologies of the Production and Utilization of Products,” September 22–26, 2008, Large Yalta, Zhukovka, Autonomous Republic of Crimea, Ukraine, Izd. Dom “Akademperiodika” NAN Ukrainy, Kiev (2008), p. 342.

  2. I. P. Smyaglikov, I. I. Filatova, L. E. Krat’ko, S. V. Goncharik, N. I. Chubrik, and V. V. Chuprasov, Spectroscopic diagnostics of a supersonic plasma jet in an air flow, in: Proc. VII Symp. of Belarus and Serbia on Physics and Diagnostics of a Laboratory and Astrophysical Plasma, September 22–26, 2008, Minsk, Republic of Belarus, Kovcheg, Minsk (2008), pp. 220–223.

  3. V. A. Ostapenko and A. V. Solotchin, Force action of a supersonic underexpanded jet on a plane barrier, Izv. SO Akad. Nauk SSSR, Ser. Tekh. Nauk, No. 3, 26–32 (1974).

    Google Scholar 

  4. N. F. Krasnov, Principles of Aerodynamic Calculation [in Russian], Vysshaya Shkola, Moscow (1981).

    Google Scholar 

  5. V. V. Lunev, Hypersonic Aerodynamics [in Russian], Mashinostroenie, Moscow (1975).

    Google Scholar 

  6. I. P. Ginzburg, Aerogasdynamics [in Russian], Vysshaya Shkola, Moscow (1966).

    Google Scholar 

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Authors and Affiliations

  1. A. V. Luikov Heat and Mass Transfer Institute, National Academy of Sciences of Belarus, 15 P. Brovka Str., Minsk, 220072, Belarus

    V. V. Chuprasov & M. S. Tret’yak

  2. Federal State Unitary Enterprise “S. A. Lavochkin Research-Production Association”, 24 Leningradskaya Str., Khimki of Moscow Region, 141400, Russia

    A. F. Klishin

Authors
  1. V. V. Chuprasov
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  2. M. S. Tret’yak
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  3. A. F. Klishin
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Corresponding author

Correspondence to V. V. Chuprasov.

Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 84, No. 5, pp. 1040–1045, September–October, 2011.

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Chuprasov, V.V., Tret’yak, M.S. & Klishin, A.F. Characteristic features of diagnostics of supersonic high-temperature jet parameters. J Eng Phys Thermophy 84, 1120–1125 (2011). https://doi.org/10.1007/s10891-011-0575-8

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  • DOI: https://doi.org/10.1007/s10891-011-0575-8

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