Calculation procedure of aerodynamic characteristics of the combined carrying system of the aircraft

Aviation technics and technology


Golovkin M. A.*, Kochish S. I., Kritsky B. S.**

Central Aerohydrodynamic Institute named after N.E. Zhukovsky, TsAGI, 1, Zhukovsky str., Zhukovsky, Moscow Region, 140180, Russia



Within the limits of the vortex theory the design procedure of non-stationary aerodynamic characteristics of carrying system «the central body - blades» convertible aircraft is considered. Comparison of calculation results vs the experiments data and calculations by other techniques is given.Examples of calculations are given.


rotary-wing aircraft, carrying system, the central body, blades, aerodynamic characteristics

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