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

Authors

  • Григорий Григорьевич Бильченко Kazan National Research Technical University (KNRTU-KAI) named after A. N. Tupolev
  • Наталья Григорьевна Бильченко Kazan National Research Technical University (KNRTU-KAI) named after A. N. Tupolev

DOI:

https://doi.org/10.17308/sait.2019.2/1286

Keywords:

control, heat and mass transfer, laminar boundary layer, hypersonic flows, permeable surfaces, linear temperature factor, constant blowing, 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 temperature factor and constant blowing and magnetic field for the entire segment of control is considered. The dependences of mathematical model parameters, local heat and mass transfer and friction characteristics, local blowing system power on controls are obtained. The computational experiments results are presented.

Author Biographies

  • Григорий Григорьевич Бильченко, Kazan National Research Technical University (KNRTU-KAI) named after A. N. Tupolev

    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 temperature factor and constant blowing and magnetic field for the entire segment of control is considered. The dependences of mathematical model parameters, local heat and mass transfer and friction characteristics, local blowing system power on controls are obtained. The computational experiments results are presented.

  • Наталья Григорьевна Бильченко, Kazan National Research Technical University (KNRTU-KAI) 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

2019-03-18

Issue

No. 2 (2019): April - June

Section

Mathematical Methods of System Analysis and Management

License

Условия передачи авторских прав in English

How to Cite

Analysis of the influence of linear temperature factor and constant blowing on the parameters of the mathematical model and 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, 2, 15-22. https://doi.org/10.17308/sait.2019.2/1286

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