Russian Aeronautics

, Volume 61, Issue 2, pp 183–186 | Cite as

A Method for Designing the Helicopter Skid Landing Gear by a Criterion of Landing Impact Energy Absorption

  • D. V. Nedel’koEmail author
  • S. A. Alimov
Structural Mechanics and Strength of Flight Vehicles


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.


helicopter spring skid landing gear autorotation landing efficiency coefficient plastic deformations 


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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  1. 1.Tupolev Kazan National Research Technical UniversityKazanRussia
  2. 2.PAO Kazan HelicoptersKazanRussia

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