Aerodynamic state diagnosing method of aircraft with thermal field usage
DOI :
https://doi.org/10.15587/2313-8416.2014.29267Mots-clés :
external contour, damage, plane, aircraft, temperature gradient, thermal method, boundary layer, diagnosticsRésumé
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.
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(c) Tous droits réservés Vasyl Kazak, Dmitro Shevchuk, Andrii Babenko, Mykhailo Levchenko 2014
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