E. I. Nikolaev, Maria Nikolaeva
Abstract
The numerical method for calculating the induced velocities of the helicopter rotor was developed based on Shaidakov’s disk theory. The numerical experiments were performed to test and estimate the method developed.
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The numerical method for calculating the induced velocities of the helicopter rotor was developed based on Shaidakov’s disk theory. The numerical experiments were performed to test and estimate the method developed.
Key concepts: Rotor (electric), Helicopter rotor, Vortex, Mechanics, Physics, Angular velocity, Numerical analysis, Aerospace engineering