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

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.

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Bibliographic Details
Published in:Russian aeronautics 2018-04, Vol.61 (2), p.183-186
Main Authors: Nedel’ko, D. V., Alimov, S. A.
Format: Article
Language:English
Subjects:
Automotive Engineering
Criteria
Energy absorption
Engineering
Helicopter design
Landing gear
Structural Mechanics and Strength of Flight Vehicles
Online Access:Get full text
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Description
Summary: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799818020058