Aerodynamic state diagnosing method of aircraft with thermal field usage

Authors

  • Vasyl Kazak National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058, Ukraine
  • Dmitro Shevchuk National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058, Ukraine
  • Andrii Babenko National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058, Ukraine
  • Mykhailo Levchenko National Aviation University pr., Komarova 1, Kyiv, Ukraine, 03058, Ukraine

DOI:

https://doi.org/10.15587/2313-8416.2014.29267

Keywords:

external contour, damage, plane, aircraft, temperature gradient, thermal method, boundary layer, diagnostics

Abstract

The method of aerodynamic condition of the aircraft on the thermal fields was developed as a research result. Based on the mathematical and natural experiments, there are identified the regularities of formation of temperature gradients in the boundary layer of air that occurs after damage of external contours; there are detected parameters that affect the behavior of the temperature gradient arising from damage.

Author Biographies

Vasyl Kazak, National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058

Doctor of Technical Sciences, Professor

Automation and Energy Management Department

Dmitro Shevchuk, National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058

PhD, Associate Professor

Automation and Energy Management Department

Andrii Babenko, National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058

PhD, Assistant Professor

Air Transportation Management Department

Mykhailo Levchenko, National Aviation University pr., Komarova 1, Kyiv, Ukraine, 03058

Department of Automation and Energy Management 

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Published

2014-11-24

Issue

Section

Technical Sciences