Aerodynamic state diagnosing method of aircraft with thermal field usage
<p>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...
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PC Technology Center
2014-11-01
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| Series: | ScienceRise |
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| Online Access: | http://journals.uran.ua/sciencerise/article/view/29267 |
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doaj-c343bcb24e234ccf9dcc9a73d62d46232020-11-25T01:55:15ZengPC Technology CenterScienceRise2313-62862313-84162014-11-0142(4)818910.15587/2313-8416.2014.2926729099Aerodynamic state diagnosing method of aircraft with thermal field usageVasyl Kazak0Dmitro Shevchuk1Andrii Babenko2Mykhailo Levchenko3National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058National Aviation University Komarova Ave, 1, Kiev, Ukraine, 03058National Aviation University pr., Komarova 1, Kyiv, Ukraine, 03058<p>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.</p>http://journals.uran.ua/sciencerise/article/view/29267external contourdamageplaneaircrafttemperature gradientthermal methodboundary layerdiagnostics |
| collection |
DOAJ |
| language |
English |
| format |
Article |
| sources |
DOAJ |
| author |
Vasyl Kazak Dmitro Shevchuk Andrii Babenko Mykhailo Levchenko |
| spellingShingle |
Vasyl Kazak Dmitro Shevchuk Andrii Babenko Mykhailo Levchenko Aerodynamic state diagnosing method of aircraft with thermal field usage ScienceRise external contour damage plane aircraft temperature gradient thermal method boundary layer diagnostics |
| author_facet |
Vasyl Kazak Dmitro Shevchuk Andrii Babenko Mykhailo Levchenko |
| author_sort |
Vasyl Kazak |
| title |
Aerodynamic state diagnosing method of aircraft with thermal field usage |
| title_short |
Aerodynamic state diagnosing method of aircraft with thermal field usage |
| title_full |
Aerodynamic state diagnosing method of aircraft with thermal field usage |
| title_fullStr |
Aerodynamic state diagnosing method of aircraft with thermal field usage |
| title_full_unstemmed |
Aerodynamic state diagnosing method of aircraft with thermal field usage |
| title_sort |
aerodynamic state diagnosing method of aircraft with thermal field usage |
| publisher |
PC Technology Center |
| series |
ScienceRise |
| issn |
2313-6286 2313-8416 |
| publishDate |
2014-11-01 |
| description |
<p>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.</p> |
| topic |
external contour damage plane aircraft temperature gradient thermal method boundary layer diagnostics |
| url |
http://journals.uran.ua/sciencerise/article/view/29267 |
| work_keys_str_mv |
AT vasylkazak aerodynamicstatediagnosingmethodofaircraftwiththermalfieldusage AT dmitroshevchuk aerodynamicstatediagnosingmethodofaircraftwiththermalfieldusage AT andriibabenko aerodynamicstatediagnosingmethodofaircraftwiththermalfieldusage AT mykhailolevchenko aerodynamicstatediagnosingmethodofaircraftwiththermalfieldusage |
| _version_ |
1724984188565716992 |