Author:
Zagidulin A R,Podruzhin E G
Abstract
Abstract
The article describes the design and computation of the aircraft landing gear with an electromagnetic-gas shock absorber. A numerical simulation of the landing impact was carried out at different values of the initial vertical velocity. The dependence of the optimal electric current in the winding of the shock absorber electromagnet on the vertical speed is obtained.
Cited by
2 articles.
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