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Simulation of Supersonic Flow in a Channel with a Step on Nonstructured Meshes with the Use of the Weno Scheme

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Journal of Engineering Physics and Thermophysics Aims and scope

An Erratum to this article was published on 23 November 2015

Results of modeling of the temperature and stressed-strained states of the reflector of a mirror space antenna installed on a spacecraft that conducts a flight on geostationary and low near-earth orbits have been presented.

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References

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Authors and Affiliations

  1. N. É. Bauman State Technical University, 5 2ya Baumanskaya Str., Moscow, 105005, Russian

    S. V. Reznik, P. V. Prosuntsov & A. V. Azarov

Authors
  1. S. V. Reznik
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  2. P. V. Prosuntsov
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  3. A. V. Azarov
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Correspondence to S. V. Reznik.

Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 88, No. 4, pp. 945–950, July–August, 2015.

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Reznik, S.V., Prosuntsov, P.V. & Azarov, A.V. Simulation of Supersonic Flow in a Channel with a Step on Nonstructured Meshes with the Use of the Weno Scheme. J Eng Phys Thermophy 88, 877–884 (2015). https://doi.org/10.1007/s10891-015-1263-x

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  • DOI: https://doi.org/10.1007/s10891-015-1263-x

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