Simulation and optimization of ultralight helicopter aerodynamic characteristics

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The simulation and optimization of the ultralight helicopter aerodynamic characteristics at the design stages and phases which permit to determine optimal values ​​ of the engine power and speed are performed.

Ultralight helicopter, aerodynamic characteristics, simulation, optimization

Короткий адрес: https://sciup.org/14249854

IDR: 14249854

Статья научная