Computational Research of the Main Rotor Hover and Vertical...

Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model

Ignatkin, Yu. M., Makeev, P. V., Shaidakov, V. I., Shomov, A. I.
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Volume:
61
Language:
english
Journal:
Russian Aeronautics
DOI:
10.3103/S1068799818030121
Date:
July, 2018
File:
PDF, 1.30 MB
english, 2018
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