Olena Kuchma, Vasyl Kazak, Dmytro O. Shevchuk, Oleksandr Yakushenko, И В Шевченко
Abstract
The article is dedicated to the problem of unmanned airplane wing leading edge damages influence on its integral aerodynamic characteristics. Experimental research results of a vortex system formed as a result of the damage are described.
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The article is dedicated to the problem of unmanned airplane wing leading edge damages influence on its integral aerodynamic characteristics. Experimental research results of a vortex system formed as a result of the damage are described.
Key concepts: Wing, Aerodynamics, Airplane, Leading edge, Aerospace engineering, Enhanced Data Rates for GSM Evolution, Vortex, Front (military)