Abstract This paper presents the results of calculating the energy criterion being proposed by an example of two types of skid landing gear for a multipurpose helicopter of transport category.
A Method for Designing the Helicopter Skid Landing Gear by a Criterion of Landing Impact Energy Absorption
Russian Aeronautics ; 61 , 2 ; 183-186
2018-04-01
4 pages
Article (Journal)
Electronic Resource
English