Analysis of the influence of linear decreasing blowing and linear increasing temperature factor on the parameters of the mathematical modeland local characteristics of heat and mass transfer and friction on the permeable surfacesof the hypersonic aircraft

Authors

  • Grigorij Grigorievich Bilchenko Kazan National Research Technical University (KNRTU­KAI) named after A. N. Tupolev
  • Natalya Grigorievna Bilchenko Kazan National Research Technical University (KNRTU­KAI) named after A. N. Tupolev

DOI:

https://doi.org/10.17308/sait.2019.4/2676

Keywords:

control, heat and mass transfer, laminar boundary layer, hypersonic flows, permeable surfaces, linear decreasing blowing, linear increasing temperature factor, mathematical model parameters, local heat and mass transfer and friction characteristics

Abstract

The properties of mathematical model of heat and mass transfer and friction control in laminar boundary layer on permeable cylindrical and spherical surfaces of hypersonic aircraft are investigated. The case of application of a combination of linear decreasing blowing, linear in-creasing temperature factor and constant magnetic field for the entire segment of control is considered. The dependences of mathematical model parameters, local heat and mass transfer and friction characteristics on controls are obtained. The computational experiments results are presented.

Author Biographies

  • Grigorij Grigorievich Bilchenko, Kazan National Research Technical University (KNRTU­KAI) named after A. N. Tupolev

    Candidate of Science in Physics and Mathematics, Researcher of Laboratory of Modeling of Physical and Technical Processes, Department of Heat Engineering and Power Engineering Machinery, Kazan National Research Technical University (KNRTU-KAI) named after A. N. Tupolev

  • Natalya Grigorievna Bilchenko, Kazan National Research Technical University (KNRTU­KAI) named after A. N. Tupolev

    Candidate of Science in Physics and Mathematics, Researcher of Laboratory of Modeling of Physical and Technical Processes, Department of Heat Engineering and Power Engineering Machinery, Kazan National Research Technical University (KNRTU-KAI) named after A. N. Tupolev

References

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Published

2019-09-23

Issue

No. 4 (2019): October - December

Section

Mathematical Methods of System Analysis and Management

License

Условия передачи авторских прав in English

How to Cite

Analysis of the influence of linear decreasing blowing and linear increasing temperature factor on the parameters of the mathematical modeland local characteristics of heat and mass transfer and friction on the permeable surfacesof the hypersonic aircraft. (2019). Proceedings of Voronezh State University. Series: Systems Analysis and Information Technologies, 4, 13-20. https://doi.org/10.17308/sait.2019.4/2676

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