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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Contributors:

    Published in:

    Russian Aeronautics ; 61 , 2 ; 183-186


    Publication date :

    2018-04-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    HELICOPTER SKID LANDING GEAR

    LARKIN III JOHN C / WARD EMERY N / SUMNER WILLIAM P et al. | European Patent Office | 2019

    Free access

    HELICOPTER SKID LANDING GEAR

    BERNIER SIMON / FEWS ROBERT CLIVE / GUILLOT MICHEL et al. | European Patent Office | 2017

    Free access

    Helicopter skid landing gear

    LARKIN III JOHN C / WARD EMERY N / SUMNER WILLIAM P et al. | European Patent Office | 2020

    Free access

    HELICOPTER SKID LANDING GEAR

    AMANTE WILLIAM A | European Patent Office | 2016

    Free access