Shock wave-boundary layer interactions at the supersonic flow around three-dimensional configurations

Authors

  • Євген Миколайович Панов National Technical University of Ukraine "Kyiv Polytechnic Institute" Peremogy ave., 37, Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0002-4885-2777
  • Антон Янович Карвацький National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0003-2421-4700
  • Сергій Володимирович Лелека National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0002-4372-9454
  • Тарас Валерійович Лазарєв National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0001-8260-1683
  • Анатолій Юрійович Педченко National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056, Ukraine https://orcid.org/0000-0001-5065-5003

DOI:

https://doi.org/10.15587/1729-4061.2015.50911

Keywords:

supersonic flow, boundary layer, shock wave, interference of configurations, numerical analysis

Abstract

The study suggests that the problems of interactions of turbulent flows at the supersonic flow around aircraft elements be solved by numerical analysis methods aided by a mathematical model that is based on the system of the Reynolds-averaged Navier-Stokes equations. The system includes the k-ω SST turbulence model for viscous compressible medium (with two scalar equations of turbulent kinetic energy and relative velocity of its dissipation with the modification that takes into account the transfer of shear stress). The paper presents applied testing and verification of the model along with examples of the problems on supersonic flows around a flat wall and a sphenoid superstructure as well as a perpendicular gas stream. We have identified physical characteristics of interactions between the condensation wave and the boundary turbulent layer, which manifest themselves in the formation of a complex structure of disconnecting and connecting zones of a boundary turbulent layer, which are characterized by respective lines of separation and joining on the wrap surface. The solutions adequately reflect the pattern of the supersonic flow of a compressible medium, condensation waves and vortex zones that are commonly observed during field studies. The comparative analysis of the results of numerical modeling and experimental data confirms the applicability of the mathematical model for complex tasks of the supersonic gas-dynamic state.

Author Biographies

Євген Миколайович Панов, National Technical University of Ukraine "Kyiv Polytechnic Institute" Peremogy ave., 37, Kyiv, Ukraine, 03056

Doctor of Engineering, professor

The chemical, polymer and silicate machine engineering department

Антон Янович Карвацький, National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056

Doctor of Engineering, Professor

Chemical, polymer and silicate machine engineering department

Сергій Володимирович Лелека, National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056

PhD, postdoctoral research fellow

Research center «Resource-saving technologies»

Тарас Валерійович Лазарєв, National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056

PhD, postdoctoral research fellow

Chemical, polymer and silicate machine engineering department

Анатолій Юрійович Педченко, National Technical University of Ukraine "Kyiv Polytechnic Institute" 37 Peremogy ave., Kyiv, Ukraine, 03056

Postgraduate student

Chemical, polymer and silicate machine engineering department

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Published

2015-10-23

How to Cite

Панов, Є. М., Карвацький, А. Я., Лелека, С. В., Лазарєв, Т. В., & Педченко, А. Ю. (2015). Shock wave-boundary layer interactions at the supersonic flow around three-dimensional configurations. Eastern-European Journal of Enterprise Technologies, 5(4(77), 4–11. https://doi.org/10.15587/1729-4061.2015.50911

Issue

Vol. 5 No. 4(77) (2015): Mathematics and Cybernetics - applied aspects

Section

Mathematics and Cybernetics - applied aspects

License

Copyright (c) 2015 Евгений Николаевич Панов, Антон Янович Карвацький, Сергій Володимирович Лелека, Тарас Валерійович Лазарєв, Анатолій Юрійович Педченко

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