| Autor: |
Kruchinin, M. M., Artamonov, B. L. |
| Zdroj: |
Russian Aeronautics; Oct2021, Vol. 64 Issue 4, p636-645, 10p |
| Abstrakt: |
The main provisions of the methodology for calculating the landing of a helicopter on a tricycle wheeled landing gear, taking into account all the necessary design features of this type of landing gear and the peculiarities of the main rotor near the ground surface, are described. The comparison of computational studies with experimental data obtained during flight tests of the Mi-38 helicopter is presented. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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